Aeronautics

Resource Information

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

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

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

100+ Items that share the Concept Aeronautics

Context

Subject of

Aeronautics

Resource Information

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