Browse TRAIL Inventories

A method for the design of sweptback wings warped to produce specified flight characteristics at supersonic speeds

NACA transonic wind-tunnel test sections

Measurement and analysis of wing and tail buffeting loads on a fighter airplane

Ideal temperature rise due to constant-pressure combustion of a JP-4 fuel

On the Kernel function of the integral equation relating the lift and downwash distributions of oscillating finite wings in subsonic flow

Determination of lateral-stability derivatives and transfer-function coefficients from frequency-response data for lateral motions

Longitudinal Aerodynamic Characteristics and Effect of Rocket Jet on Drag of Models of the Hermes A-3A and A-3B Missiles in Free Flight at Mach Numbers From 0.6 to 2.0

A comparative analysis of the performance of long-range hypervelocity vehicles

Bodies of revolution having minimum drag at high supersonic airspeeds

Stability and control characteristics obtained during demonstration of the Douglas X-3 research airplane

Some aspects of the design of hypersonic boost-glide aircraft

Performance of a high-solidity high-pressure-ratio transonic rotor

Performance measurements from a rocket-powered exploratory research missile flown to a Mach number of 10.4

Pressure-drop characteristics of a 22-segment mock-up of the General Electric Company air-cooled aircraft reactor

The pressure-recovery and propeller-force characteristics of a propeller-spinner-cowling combination employing NACA 4-(5) (05)-037 six- and eight-blade dual-rotation propellers with an NACA 1 series D-type cowl

Stall and flame-out resulting from firing of armament

Stability and drag characteristics of 1/10-scale model of the Convair XF2Y-1 airplane with open inlets containing boundary layer splitter plates as obtained in free flight at Mach numbers between 0.7 and 1.5 : TED No. NACA DE 365

Engine performance of precision-forged, electropolished and machined blades of Nimonic 80 and 80A alloys

Experimental drag coefficients of round noses with conical windshields at Mach number 2.72

Effect of inlet-air baffles on rotating-stall and stress characteristics of an axial-flow compressor in a turbojet engine

Effect of inlet flow distortion on compressor stall and acceleration characteristics of a J65-B-3 turbojet engine

The effect of inlet installation on the zero-lift drag of a 60 degree delta-wing-body configuration from flight tests at Mach numbers from 0.8 to 1.86

A flight investigation at transonic speeds of a model having a triangular wing of aspect ratio 2

A flight investigation at transonic speeds of a model having a triangular wing of aspect ratio 3

Effect of surface-active additives on physical properties of slurries of vapor-process magnesium

Design procedure for transpiration-cooled strut-supported turbine rotor blades

An air-borne target simulator for use in optical sight tracking studies

Investigation of the effects of bomb-bay configuration upon the aerodynamic characteristics of a body with circular cross section at supersonic speeds

Experimental performance of the mixed-oxides-of-nitrogen-ammonia propellant combination in a 1000-pound-thrust rocket engine

Rocket-engine throttling

Experimental rocket performance with 15 percent fluorine - 85 percent oxygen and JP4

Wing-load measurements at supersonic speeds of the Douglas D-558-II research airplane

Preliminary investigation of the effects of altitude and inlet-pressure distortions on steady-state and surge fuel flow of the J57-P-1 turbojet engine

Investigation of the effects of body indentation and of wing-plan-form modification on the longitudinal characteristics of a 60 degree swept-wing-body combination at Mach numbers of 1.41, 1.61, and 2.10

Preliminary investigation of some internal boundary-layer-control systems on a side inlet at Mach number 2.96

Some effects of propeller operation and location on ability of a wing with plain flaps to deflect propeller slipstreams downward for vertical take-off

A study of the application of airfoil section data to the estimation of the high-subsonic-speed characteristics of swept wings

A study of local-pressure fluctuations relative to static-pressure distributions on two-dimensional airfoils at high subsonic Mach numbers

A Study of the Correlation Between Flight and Wind-Tunnel Buffeting Loads

Preliminary performance data of several tail-pipe-cascade-type model thrust reversers

Review of status, methods and potentials of gas-turbine air-cooling

Thrust and drag characteristics of simulated variable-shroud nozzles with hot and cold primary flows at subsonic and supersonic speeds

Transonic free-flight investigation of the longitudinal aerodynamic characteristics of a 1/10-scale steel-wing of the Northrop MX-775A missile with leading-edge extensions, inboard trailing-edge flaps, and a speed brake on the vertical tail

Wing-load measurements of the Bell X-5 research airplane at a sweep angle of 58.7 degrees

Analytical and experimental study of transient-response characteristics of a turboprop engine

Analysis of V-G records from ten types of Navy airplanes in squadron operations during the period 1949 to 1953

Theoretical pressure distributions for some slender wing-body combinations at zero lift

Aerodynamic characteristics at Mach numbers from 0.7 to 1.75 of a four-engine swept-wing airplane configuration as obtained from a rocket-propelled model test

Aerodynamic heating of rocket-powered research vehicles at hypersonic speeds

An experimental investigation at a Mach number of 2.01 of the effects of body cross-section shape on the aerodynamic characteristics of bodies and wing-body combinations


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