Browse TRAIL Inventories

Analysis of Rocket, Ram-Jet, and Turbojet Engines for Supersonic Propulsion of Long-Range Missiles 2 - Rocket Missile Performance

Note on the Effects of First-Order Aerodynamic Loads on Propeller Shaft Loads with Emphasis on Counterrotating Propellers

Preliminary Investigation of the Static Longitudinal and Lateral Stability Characteristics of a 0.05-Scale Model of the Convair F2Y-1 Airplane at High Subsonic Speeds

High-Speed Drag and Opening Characteristics of a Kaman Rotochute Model

Vapor pressures and calculated heats of vaporization of concentrated nitric acid solutions in the composition range 71 to 89 percent nitrogen dioxide, 1 to 10 percent water, and in the temperature range 10 to 60 degrees C

A flight evaluation of the stability and control of the X-4 swept-wing semitailless airplane

Flight determination of the drag of conical-shock nose inlets with various cowling shapes and axial positions of the center body at Mach numbers from 0.8 to 2.0

Exploratory engine test of transpiration-cooled turbine-rotor blade with wire-cloth shell

High-altitude performance of an experimental turbular prevaporizing combustor

Investigation of impulse-type supersonic compressor with hub-tip ratio of 0.6 and turning to axial direction I : performance of rotor alone

Investigation of a trailing-edge paddle-control surface on a triangular wing of aspect ratio 2 at subsonic and supersonic speeds

Investigation of a supersonic-compressor rotor with turning to axial direction II : rotor component off-design and stage performance

Investigation of a translating-cone inlet at Mach numbers from 1.5 to 2.0

Internal performance at Mach number to 2.0 of two auxiliary inlets immersed in fuselage boundary layer

Investigation of a high-temperature single-stage turbine suitable for air cooling and turbine stator adjustment 1: design of vortex turbine and performance with stator at design setting

Investigation of a high-temperature single-stage turbine suitable for air cooling and turbine stator adjustment 2: performance of vortex turbine at various stator settings

Investigation of a high-pressure ratio eight-stage axial-flow research compressor with two transonic inlet stages III : individual stage performance characteristics

Investigation of a missile airframe with control surfaces consisting of projecting quadrants of the nose cone

Investigation of a 10-stage subsonic axial-flow research compressor V : effect of reducing inlet-guide-vane turning on over-all and inlet-stage performance

Investigation of a 10-stage subsonic axial-flow research compressor VI : performance evaluation and flow distributions in the first, fifth, and tenth stages

An investigation of a supersonic aircraft configuration having a tapered wing with circular-arc sections and 40 degree sweepback : aerodynamic characteristics of the configuration equipped with a canard control surface at a Mach number of 1.89

Investigation of Supersonic-Compressor Rotors Designed with External Compression

Investigation of three highly loaded subsonic-inlet-stage axial-flow compressors employing varying radial gradients of energy addition

Investigation of three low-temperature-ratio combustor configurations in a 48-inch-diameter ram-jet engine

Investigation of transient combustion characteristics in a single tubular combustor

Investigation to Mach number 2.0 of shock-positioning control systems for a variable-geometry inlet in combination with a J34 turbojet engine

A method for increasing the effectiveness of stabilizing surfaces at high supersonic Mach numbers

Method for studying helicopter longitudinal maneuver stability

Thrust and pumping characteristics of a series of ejector-type exhaust nozzles at subsonic and supersonic flight speeds

Pressure distributions on triangular and rectangular wings to high angles of attack Mach numbers 1.45 and 1.97

Performance of isentropic nose inlets at Mach number of 5.6

Performance of two air-cooled turbojet engines determined analytically from engine component performance for a range of cooling-air weight flows

Performance of wedge-type boundary layer diverters for side inlets at supersonic speeds

Optimum lifting bodies at high supersonic airspeeds

Organophosphorus compounds in rocket-engine applications

Performance of mixed-flow impeller, model MFI-1B, with diffuser vanes at equivalent impeller speeds from 1100 to 1700 feet per second

Performance of five low-temperature-ratio ram-jet combustors over range of simulated altitudes

Tests in the Ames 40- by 80-foot wind tunnel of the effects of varying wing modifications on the longitudinal characteristics of two-triangular wing airplane models with and without horizontal tails

Matrix methods for determining the longitudinal-stability derivatives of an airplane from transient flight data

Jet effects on pressure loading of all-movable horizontal stabilizer

Wind pressure distributions at low lift for the XF-92A delta-wing airplane at transonic speeds

Preliminary investigation of a technique for stability studies of a self-propelled model of a submerged submarine

Preliminary investigation of an asymmetric swept nose inlet of circular projection at Mach number 3.85

A preliminary study of the preparation of slurry fuels from vaporized magnesium

Preliminary wind tunnel investigation of two types of jet-exit configurations for control of aircraft

Preliminary investigation at subsonic and transonic speeds of the aerodynamic characteristics of a biplane composed of a sweptback and a sweptforward wing joined at the tips

Preliminary drag measurements of the consolidated Vultee XF-92A delta-wing airplane in flight tests to a Mach number of 1.01

Lift and drag characteristics of the Douglas X-3 research airplane obtained during demonstration flights to a Mach number of 1.20

Lateral control characteristics of two structural similar flexible wings with 45 degrees sweep: a sweptback wing and a wing with M plan form

Lift and drag characteristics of the Douglas D-558-II research airplane obtained in exploratory flights to a Mach number of 2.0


Published Year

Subject

Author

‹‹ previous 1 2 ... 64 65 66 67 68 69 70 ... 143 144 next ››