#
Aeronautics
Resource Information
The concept ** Aeronautics** represents the subject, aboutness, idea or notion of resources found in **Internet Archive - Open Library**.

The Resource
Aeronautics
Resource Information

The concept

**Aeronautics**represents the subject, aboutness, idea or notion of resources found in**Internet Archive - Open Library**.- Label
- Aeronautics

## Context

Context of Aeronautics#### Subject of

- A Fortran program to solve the steady-state matrix Riccati equation of optimal control
- A Kalman filter application to the advanced tactical inertial guidance system of the air-launched low volume ramjet cruise missile
- A London encyclopaedia, or universal dictionary of science, art, literature and practical mechanics : comprising a popular view of the present state of knowledge : illustrated by numerous engravings, a general atlas, and appropriate diagrams
- A Program Manager's handbook for system safety and Military Standard 882B
- A case study of a combat aircraft's single hit vulnerability
- A case study of a combat helicopter's single hit vulnerability
- A circular sandwich plat, transversely loaded
- A color schlieren study of ammonium perchlorate and ammonium perchlorate-binder sandwich combustion
- A comparison of buffer strip and non-buffer strip joint designs
- A comparison of computer warhead-target endgame simulations and recommendations pertaining to future endgame programs
- A comparison of optimal control theory predictions with actual pilot performance in a helicopter longitudinal tracking task
- A comparison of predicted and observed gas turbine performance
- A comparison of several finite difference equations for the displacement of a taut string subjected to a transverse load
- A comparison of solid fuel ramjet flow characteristics and combustion behavior
- A comparison of steepest-ascent and second variational techniques in solving a restricted class of trajectory optimization problems
- A comparison of the jet augmentation resulting from steady and pulsating primary flow
- A computational method for wings of arbitrary planform
- A computer aided method for the measurement of fiber diameters by laser diffraction
- A computer analysis for the determination of electrode voltage losses in magnetohydrodynamic-generator plasmas
- A computer analysis of the plasma-boundary layer behavior over a positive electrode
- A computer code (USPOTF2) for unsteady incompressible flow past two airfoils
- A computer graphics simulation of the endgame in aircraft combat survivability
- A computer program to model the Cn optical turbulence characteristics of a given atmosphere, its conversion to IBM Fortran and utilization
- A computer study of air defense gun effectiveness
- A computer study of the buckling of an imperfect cylindrical shell
- A computerized data reduction program for the Cessna 310H aircraft
- A concept of anti-satellite terminal guidance
- A conceptual design of a lighter-than-air test and research vehicle
- A critical analysis of fatigue-crack propagation data for 2024-T3 aluminum
- A critical study of spin-up drag loads on aircraft landing gears
- A cruise control instrument for tactical turbojet aircraft
- A design criterion for arbitrary diffusers
- A design of an annular cascade tunnel and a cascade of airfoils
- A digital computer study of the buckling of actual imperfect cylinders : a modification of the computer program SATANS - theory and user's model for SATANS - I and SATANS - II
- A digital computer study of the buckling of shallow spherical caps and truncated hemispheres
- A digital computer study of the first-stage trajectories of high initial acceleration rockets
- A digital-analog computer control for use in an aerodynamic heat simulation system
- A discrete protential element approach to nonsteady subsonic lifting surface theory
- A feasibility study for a backup flight control system for the A7A/B aircraft
- A feedback system for automatic control of simulated aerodynamic heating
- A fiber optic pressure transducer
- A fixed -base variable-stability carrier approach landing simulator (CALS)
- A flight test determination of the static and dynamic longitudinal stability of the Cessna 310H aircraft
- A flight test determination of the static longitudinal stability of the Cessna 310d airplane
- A gas turbine combustor test facility for fuel composition investigations
- A guide to and an abstracted bibliography of aircraft side-arm control stick research
- A heat flow measurement system for a radiant heat test facility
- A heat transfer model of a heated helium airship
- A high enthaply [i.e., enthalpy] test facility powered by a gaseous core reactor
- A holographic investigation of particulates in metallized solid fuel ramjet combustion
- A hot-wire anemometer study of free turbulent mixing in axial, pressure gradients
- A investigation of the effects of a sharp velocity gradient on the flexure-torsion flutter speed of an airfoil
- A literature survey of the problem of aircraft spins
- A mapping of the viscous flow behavior in a controlled diffusion compressor cascade using laser doppler velocimetry and preliminary evaluation of codes for the prediction of stall
- A mathematical model for the longitudinal control system of the space shuttle orbiter
- A method for three-dimensional flow analysis in a rotor using a high speed digital computer
- A method of predicting the performance of axial flow turbines using a digital computer to develop performance maps
- A method to calculate the parameters of wings of arbitrary planform
- A microcomputer program package of the USAF stability and control DATCOM
- A microprocessor controlled automatic data logging system (ADL)
- A microprocessor-controlled data acquisition system for the Federal Scientific Model UA-500-1 ubiquitous spectrum analyzer
- A microprogrammable data acquisition and control system (MIDAS IIA) with application to mean meteorological data
- A missile flyout model for ISEAS
- A model based technique for flight director design : helicopter hovering flight
- A modified design concept, utilizing deck motion prediction, for the A-7E automatic carrier landing system
- A new approach to pilot rating scales
- A new method of correlation signal damping
- A new optimization theory for the end-initiated linear shaped charge
- A new parameter optimization method applied to autopilot design
- A numerical analysis of pipe flow stability
- A numerical investigation of finite-amplitude disturbances in a plane Poiseuille flow
- A parameter optimization approach to aircraft gust alleviation
- A parametric investigation of soot behavior and other emissions in a gas turbine combustor
- A personalized system of instruction for aircraft performance
- A personalized system of instruction for gas dynamics
- A pilot evaluation of movable and rigid aircraft controls
- A piloted simulation investigating handling qualities and performance requirements of a single-pilot helicopter in air combat employing a helmet-driven turreted gun
- A preliminary design and longitudinal dynamics study of a VTOL aircraft to operate efficiently in low altitude high speed flight
- A preliminary design study for a ground effect machine
- A preliminary evaluation of the evaluation of the NAvion as a lateral as a lateral-directional flight simulator for use in the investigation of flying qualities criteria
- A preliminary feasibility study for the utilization of a tilt-rotor aircraft (MV-22) for logistical support to the military outpost along the Venezuelan jungle area bordering Colombia
- A preliminary investigation of aural input/output systems for in-flight information retrieval
- A preliminary investigation of the use of lift control in maneuvering flight
- A pressure control system for a hypersonic wind tunnel
- A program for the stability analysis of pipe Poiseuille flow
- A proposal for helicopter vibration reduction using electro-hydraulic servo control
- A proposal for the control of propellant utilization in a liquid bipropellant rocket engine
- A radar model for the Interactive Simulation of Engagements at Sea (ISEAS)
- A rational basis for circumferential distortion index formulation
- A remotely controlled wind tunnel model for the demonstration of aircraft stability and control characteristics
- A revised design concept for the A-7E approach power compensator system
- A second-order epsilon method for constrained trajectory optimization
- A sequential strain monitor and recorder for use in aircraft fatigue life prediction
- A simplified approach to low height determination
- A simplified method for digital computation of closed loop frequency response
- A simulation investigation of Scout/Attack helicopter directional control requirements for hover and low-speed tasks
- A simulator evaluation of pilot response to an aircraft cockpit spin indicator system
- A simulator evaluation of pilot response to low frequency aircraft vibration with audio feedback
- A simulator study of a nonlinear roll damper for the F-8 airplane in the carrier approach maneuver
- A simulator study of the horizontal landing characteristics and piloting techniques for manned reentry gliders
- A stability analysis of the proposed circulation control rotor (CCR) prototype
- A state-of-the-art assessment of air data sensors for naval aircraft
- A study of an adaptive aircraft control system in a self-organizing configuration
- A study of an automatic power compensator with airspeed and angle of attack as controlling inputs
- A study of boundary layer and mass bleed in a short length supersonic diffuser for a gas dynamic laser
- A study of compressible perfect fluid motion in turbomachines with indefinitely many blades
- A study of dynamic forces in aircraft landing gear struts with relation to the optimum angle of suspension
- A study of exhaust gas temperature measurement methods
- A study of friction and detonation in geometrically similar engines
- A study of methods to increase the lift of supersonic airfoils at low speeds
- A study of pilot induced lateral-directional instabilities
- A study of porous metal cooling
- A study of pressure control for a blowdown wind tunnel
- A study of pressure drop in helical coils
- A study of pull-through failures of mechanically fastened joints
- A study of spectrum loading and range-pair counting method effects on cumulative fatigue damage
- A study of state rate feedback implicit model following control for VSTOL aircraft
- A study of supersonic cascade flutter
- A study of supersonic flow past vibrating panels and shells
- A study of supersonic flow past vibrating shells and cascades
- A study of the crack damage in fuel-filled tank walls due to ballistic penetrators
- A study of the effect of boundary layer control on an axial flow compressor stage
- A study of the effect of repeated tension impact loads upon certain metals used in aircraft construction
- A study of the effect of some non-linear stability derivatives on the lateral motions of aircraft
- A study of the effect of various fuels on the optimum length of a gas turbine combustor equipped with a vaporizer tube
- A study of the effects of rapidly applied loads and repeated loads on countersunk riveted joints
- A study of the failure of joints in composite material fuel cells due to hydraulic ram loading
- A study of the hydrodynamic impact loads on a dihedral hydrofoil suitable for seaplane use
- A study of the linear self-adaptive system
- A study of the temperature gradients of gases flowing through heated porous metal
- A study of the wake at supersonic air flow of elliptical body - flat disk combination using hydraulic analogy to compressible air flow
- A study of the world's naval surface-to-air missile defense systems
- A study of turbulent wakes in constant streamwise pressure gradients
- A study of unsteady transonic interference effects
- A survey of the pressure distribution within the plenum chamber of the XR-3 testcraft
- A temperature survey of the region aft of a cooling orifice of an air film cooled metal surface exposed to high temperature and high velocity gases
- A temperature-survey in the secondary air mixing zone of the burner of a J33-A-17 turbo jet engine
- A theoretical analysis of the application of a yaw damper servomechanism to improve lateral oscillatory stability
- A theoretical analysis of the effect of the modulus of elasticity and other paramters upon the flutter of a helicopter rotor blade in hovering flight
- A theoretical analysis of unsteady transonic cascade flow
- A theoretical examination of a re-entry capsule incorporating an autorotating rotor
- A theoretical investigation of particle motion in an oscillating gas
- A theoretical investigation of particle trajectories through a Prandtl-Meyer expansion fan
- A theoretical performance investigation of an afterburning turbofan engine : appendix
- A thermal testing facility for the Aeronautics Department at USNPS
- A trade-off study of tilt rotor aircraft versus helicopters using VASCOMP II and HESCOMP
- A user's manual and program description of SEA PLOT : a three-dimensional graphics program depicting a war-at-sea encounter between a single ship and a single aircraft
- A validation of mathematical models for turbojet test cells
- A video bandwidth communications system utilizing optical fiber transmission
- A visual approach and landing simulator system
- A visual investigation of the interaction of shock waves from a body in curvilinear diving flight by simulated surface waves on water
- A wide band acceleration measuring, recording and analyzing system
- A wind tunnel investigation of the hydrodynamic stability of a manned underwater station in ocean currents
- ATTACK vs SCAN : a comparison of endgame aircraft survivability computer programs
- Activation energies of global reactions in laminar flame propagation
- Adaptation of the improved antiaircraft artillery simulation computer program (P001) for use at the Naval Postgraduate School in aircraft combat survivability studies
- Aerial locomotion,
- Aerial navigation in warfare
- Aerial navigation.
- Aerodynamic characteristics of a wedge and cone at hypersonic mach numbers
- Aerodynamic stabilization of an electrical discharge for gas lasers
- Aerodynamically efficient gradient refractive index missile seeker lens
- Aeroelastic problems in an antenna vibration project
- Aeroelastic study of a simple model
- Aeronautical applications of holographic interferometry
- Aeronautical engineering and airplane design,
- Aeronautics : a class text
- Aeronautics in theory and experiment
- Aeronautics, a class text
- Aeroplane design, : and A simple explanation of inherent stability
- Air cooling of a horizon-tally grooved turbine blade model with covering metal sleeve
- Air cooling of a slotted gas turbine blade
- Air defense concepts and effectiveness
- Air film cooling of a metal surface exposed to high temperature and high velocity gases
- Air inlets for turbojet engines through the transonic speed range
- Air navigation for flight officers,
- Air power, naval, military, commercial
- Airborne laser turret flow control : a parametric study of wind tunnel model conditions
- Aircraft data acquisition system for flight evaluation
- Aircraft fuel tank entry wall-projectile interaction studies
- Aircraft in peace and the law,
- Aircraft, its development in war and peace and its commercial futures
- Airfare of to-day and of the future
- Airfare of to-day and of the future,
- Airships past and present, : together with chapters on the use of balloons in connection with meteorology, photography and the carrier pigeon,
- Airships past and present, : together with chapters on the use of balloons in connection with meteorology, photography and the carrier pigeon,
- All about flying
- An adaptation and validation of a primitive variable mathematical model for predicting the flows in turbojet test calls and solid fuel ramjets
- An aerodynamic performance evaluation of the NASA/Ames Research Center Advanced Concepts Flight Simulator
- An analysis of a compound pendulum rocket suspension
- An analysis of a geometric stabilization system using body fixed gyros
- An analysis of ground erosion caused by jet downwash impingement
- An analysis of symmetric reinforcement of graphite/epoxy honeycomb sandwich panels with a circular cutout under uniaxial compressive loading
- An analysis of tandem helicopter parameters
- An analysis of the effect of a flight director on pilot performance in a helicopter hovering task
- An analysis of the human transfer function in aircraft longitudinal motion
- An analysis of the performance of the fans of a wind tunnel at the Naval Postgraduate School
- An analysis of the precepts available for synthesizing feedback control system when output characteristics are specified
- An analysis of the stick fixed dynamic stability of a typical VTOL aircraft during transition flight out of ground effect
- An analysis of three approaches to the helicopter preliminary design problem
- An analytical analysis of the effects of instantaneous vorticity on compressor performance
- An analytical investigation of the ducted propeller for hydrodynamic propulsion
- An analytical technique for the design of multi-loop servomechanism compensation
- An anlytical and experimental analysis of factors affecting exhause system performance in sea level static jet engine test facilities
- An apparatus for sizing particulate matter in solid rocket motors
- An application of holographic interferometry to gun barrel erosion
- An application of the method of characteristics to axially symmetric supersonic flow
- An application of vortex generators to single slotted flap
- An approximate method of calculating three-dimensional, compressible flow in axial turbo-machines
- An effect of turbulent diffusion on the glow discharge-to-arc transition
- An elastic-plastic finite element analysis of notched aluminum panels
- An engineering study of altitude determination deficiencies of the Service Aircraft Instrumentation Package (SAIP)
- An evaluation of equipment to measure directly the skin friction forces on a flat plate
- An evaluation of the longitudinal dynamic stability of an aircraft at stall
- An evaluation of the tension impact test by correlation with the physical properties of aluminum alloys
- An experimental analysis of a cylindrical shock wave for use in a cylindrical gas dynamic laser
- An experimental analysis of environmental effects on pressure sensing systems for oscillating pressures
- An experimental analysis of the mixing of a pulsating air jet at varying frequencies in a steady air flow
- An experimental determination of the aerodynamic drag characteristics of variable geometry rigid bodies
- An experimental investigation by hypersonic flow over blunt nosed cones at a mach number of 5.8
- An experimental investigation into the forebody and engine inlet airflow characteristics of a photographic reconnaissance window pallet on the RF/A-18 aircraft
- An experimental investigation of a fighter aircraft model at high angles of attack
- An experimental investigation of a fully cavitating two-dimensional flat plate hydrofoil near and free surface
- An experimental investigation of combustion modulation techniques for a solid fuel ramjet
- An experimental investigation of combustion pressure oscillations in solid fuel ramjets
- An experimental investigation of flame propagation downstream of a cylindrical flameholder
- An experimental investigation of flame spreading from bluff body flameholders
- An experimental investigation of flow conditions behind a bluff body flameholder
- An experimental investigation of flow conditions behind a bluff body flameholder
- An experimental investigation of fuel regression rate control in solid fuel ramjets
- An experimental investigation of heat transfer rates on a blunt body in hypersonic flow
- An experimental investigation of hypersonic flow over blunt nosed cones at a Mach number of 5.8
- An experimental investigation of ignition and flame stabilization in a turbulent mixing zone
- An experimental investigation of short diffusers for gas dynamic lasers
- An experimental investigation of soot behavior in a gas turbine combustor
- An experimental investigation of soot size and flow fields in a gas turbine engine augmentor tube
- An experimental investigation of sooting characteristics of a gas turbine combustor and augmentor tube
- An experimental investigation of the combustion behavior of solid fuel ramjets
- An experimental investigation of the dual chamber rocket
- An experimental investigation of the effects of swirling air flows on the combustion properties of a solid fuel ramjet motor
- An experimental investigation of the effects of swirling and pulsing the flow through an axisymmetric duct
- An experimental investigation of the effects upon lift of a gap between wing and body of a slender wing-body combination at mach number 1.9.
- An experimental investigation of the efficiency and experiment rates of a fluidically oscillated jet
- An experimental investigation of the general instability of ring-stiffened, unpressurized, thin-walled cylinders under axial compression
- An experimental investigation of the ignition and flammability limits of various hydrocarbon fuels in a two-dimensional solid fuel ramjet
- An experimental investigation of the internal ballistics of solid fuel ramjets
- An experimental investigation of the mass distribution from the exhaust of a coaxial plasma accelerator
- An experimental investigation of the oscillations of an airfoil near a sharp velocity gradient
- An experimental investigation of the pressure loss in flow through helical coils
- An experimental investigation of the recirculation zone of laimar flames stabilized on bluff bodies at low Reynolds numbers
- An experimental investigation of the sensitization of aliphatic hydrocarbon fuels
- An experimental investigation of the whistler nozzle and an analytical investigation of a ring wing in supersonic flow
- An experimental investigation of turbojet test cell augmentors
- An experimental investigation of various metallic/polymer fuels in a two-dimensional solid fuel ramjet
- An experimental study of a vane controlled jet flap gust alleviation system
- An experimental study of flow in a nozzle designed to provide a parallel jet at supersonic speed
- An experimental study of solid propellant deflagration using high speed motion pictures and postfire residue analysis
- An experimental study of the flow of a turbulent boundary layer over a step at M[Superscript -]2.35
- An experimental study of the influence of obstructions immediately downstream from the turbine wheel on turbine performance
- An experimental study of the stability of a laminar flame
- An experimental study to determine the reduction in ultimate bending moment of a composite plate due to an internal delamination
- An experimnetal investigation of combustion pressure oscillations in bypass configured solid fuel ramjets
- An integrated propulsion-lifting surface system for high mach number operation
- An inter-continental tie determined from the observation of an artificial satellite
- An interactive computer aid for the design and analysis of linear, single input / single output digital and continuous control systems
- An interactive computer code for preliminary design of solid propellant rocket motors
- An interactive discrete controls analysis option (ORACLS) for the CONTROLS analysis package on the IBM 3033
- An interactive graphics approach to the flight deck handling problem
- An interface between the SAI-42 correlation and probability analyzer and the ASR-33 teletypewriter set
- An interface between the Scanivalve pressure acqusition device and the ASR-33 teletypewriter set
- An investigation into methods of detecting dewetted zones in solid rocket propellants using holographic interferometry
- An investigation into some of the effects of cross coupling between the longitudinal and lateral equations of motion of a fighter type aircraft at subsonic speed
- An investigation into the control limitations of a bank to turn missile in the terminal homing phase
- An investigation into the effects of fuel additives and fuel composition on soot particle size in a T63 gas turbine combustor using light transmittance and scattering techniques
- An investigation into the feasibility of using a dual-combustion mode ramjet in a high Mach number tactical missile
- An investigation into the soot production processes in a gas turbine engine
- An investigation of Bank-to-Turn missiles
- An investigation of a method for obtaining a numerical indicator of phase coherence
- An investigation of a method for unique determination of aircraft longitudinal stability derivatives from transient flight test data
- An investigation of a method of increasing the mach number range of a subsonic wind tunnel by means of an internal nozzle in the test section
- An investigation of a transonic turbine test rig
- An investigation of an air ejector with supersonic primary flow and subsonic secondary flow
- An investigation of an automatic throttle device during turning flight
- An investigation of an expanding elliptical earth escape trajectory for a low thrust space vehicle
- An investigation of an experimental technique for determining the trajectory of a water droplet in an airstream
- An investigation of compressible flows with large whirl components
- An investigation of creep in light metal alloys
- An investigation of dynamic stresses in a landing gear at a pre-determined strut angle
- An investigation of energy addition to a compressible gas via the hydraulic analogy
- An investigation of engine and test cell operating conditions on the effectiveness of smoke suppressant fuel additives
- An investigation of forced flexural torsional oscillations of a wing and the phenomenon of flutter
- An investigation of high velocity air flow in a bend
- An investigation of high velocity radial air flow
- An investigation of inspection criteria for countersunk rivets
- An investigation of methods for determining notch root stress from far field strain in notched flat plates
- An investigation of parameters effecting the vaporization of fuel under conditions encountered in a turbo-jet combustion chamber
- An investigation of particulate behavior in solid rocket motors
- An investigation of preferential interfacial reactions in nonmetalized composite solid propellant combustion
- An investigation of pressure fluctuations around a circular cylinder
- An investigation of residual stress characterization of 7075-T6 aluminum for application in fatigue analysis
- An investigation of residual stresses in simulated wing panels of 7075-T6 aluminum
- An investigation of secondary flow effects in curved channels of square cross section
- An investigation of secondary-flow phenomena and associated losses in a high-deflection turbine cascade
- An investigation of stress determination for aircraft fatigue life estimation from in-flight strain data
- An investigation of subsonic diffuser performance
- An investigation of surging in a compressor
- An investigation of the aerodynamic response of a wind anemometer
- An investigation of the combustion process in solid fuel ramjets
- An investigation of the distribution pattern of fuel sprays under conditions of interest in jet engines
- An investigation of the dynamic characteristics of a two-gyro computing system for aerodynamics-lead pursuit courses
- An investigation of the effect of a laminar body boundary layer on the body interference pressures of a wing-body combination at mach number 1.9
- An investigation of the effect of a tangential gas velocity on combustion instability
- An investigation of the effect of a turbulent boundary layer upon the lift of a wing-body combination with a gap between wing and body at mach number 1.9
- An investigation of the effect of acceleration on the burning rate of composite propellants
- An investigation of the effect of auto throttle devices on aircraft control in the carrier landing approach
- An investigation of the effect of direct water injection on detonation
- An investigation of the effect of twist on the coupled bending-torsion vibrations of a cantilever beam
- An investigation of the effectiveness of baffles in promoting mixing of a hot gas with cold air under steady flow conditions
- An investigation of the effectiveness of smoke suppressant fuel additives for turbojet applications
- An investigation of the effectiveness of smoke suppressant fuel additives for turbojet applications
- An investigation of the effects of a side control jet on the normal force, drag, and moment of an airborne body in supersonic flight
- An investigation of the effects of air temperature on benzene spray vaporization
- An investigation of the effects of the sudden extension of a dive-recovery flap on the aerodynamic characteristics of a symmetrical airfoil in two dimensional flow
- An investigation of the effects of turbulent quenching in a can-type combustion chamber
- An investigation of the effects of weight geometry and time in repeated tension impact testing
- An investigation of the elevator and rudder hinge moment parameters of an aircraft obtained by analytical, wind tunnel and flight test determination
- An investigation of the equations of motion method for the evaluation of the longitudinal dynamic stability derivatives of the F-80A from transient response data