Browse TRAIL Inventories

A simplified instrument for recording and indicating frequency and intensity of icing conditions encountered in flight

A study of effects of viscosity on flow over slender inclined bodies of revolution

A small-deflection theory for curved sandwich plates

The static longitudinal characteristics at Mach numbers up to 0.95 of a triangular-wing canard model having a triangular control

Summary of Methods for Calculating Dynamic Lateral Stability and Response and for Estimating Lateral Stability Derivatives

Summary of results obtained by transonic-bump method on effects of plan form and thickness on lift and drag characteristics of wings at transonic speeds

Hydrodynamic investigation of a 1/13-scale model of the consolidated vultee skate 7 seaplane equipped with twin hydro-skis : TED No. NACA DE 342

Effects of horizontal-tail position, area, and aspect ratio on low-speed static longitudinal stability and control characteristics of a 60 degrees triangular-wing model having various triangular-all-movable horizontal tails

Investigation at zero angle of attack of a 16-inch ram jet engine in 8- by 6-foot supersonic wind tunnel

Investigation of altitude ignition, acceleration and steady-state operation with single combustor of J47 turbojet engine

Altitude-performance and Reynolds number investigation of centrifugal-flow-compressor turbojet engine

Altitude-ignition limit of a turbojet engine using a condenser-discharge ignition system

Wire cloth as porous material for transpiration-cooled walls

A wind-tunnel investigation of the aerodynamic characteristics of a full-scale sweptback propeller and two related straight propellers

Wind-tunnel investigation of the aerodynamic characteristics of a 1/15-scale model of the Northrop MX-775A missile

Two-dimensional cascade investigation of the maximum exit tangential velocity component and other flow conditions at the exit of several turbine blade designs at supercritical pressure ratios

A two-dimensional cascade study of the aerodynamic characteristics of a turbine-rotor blade suitable for air cooling

Theoretical study of some methods for increasing the smoothness of flight through rough air

Low-speed wind-tunnel investigation of lateral control characteristics of a 60 degrees triangular-wing model having half-delta tip controls

Schlieren investigation of the wing shock-wave boundary-layer interaction in flight

Steady-state engine windmilling and engine speed decay characteristics of an axial-flow turbojet engine

Effect of initial mixture temperature on flame speed of methane-air, propane-air and ethylene-air mixtures

Flying qualities of a high-performance personal-owner airplane

Aerodynamics of slender bodies at Mach number of 3.12 and Reynolds numbers from 2 x 10(exp 6) to 15 x 10(exp 6) : body of revolution with near-parabolic forebody and cylindrical afterbody

Experimental investigation of base pressure on blunt-trailing-edge wings at supersonic velocities

Experimental investigation of an 0.8 hub-tip radius-ratio,nontwisted-rotor-blade turbine

Preliminary investigation of the pressure fluctuations in the wakes of two-dimensional wings at low angles of attack

Jet effects on pressures and drags of bodies

Preliminary investigation of use of conical flow separation for efficient supersonic diffusion

Applicability of the hypersonic similarity rule to pressure distributions which include the effects of rotation for bodies of revolution at zero angle of attack

Experimental investigation of a 16-inch impulse-type supersonic-compressor rotor

Effects of Reynolds number on the aerodynamic characteristics of a delta wing at Mach number of 2.41

Experimental investigation of air-cooled turbine blades in turbojet engine 9: evaluation of the durability of noncritical rotor blades in engine operation

Experimental investigation of air-cooled turbine blade in turbojet engine 8: rotor blades with capped leading edges

Effects of double-slotted flaps and leading-edge modifications on the low-speed characteristics of a large-scale 45 degrees swept-back wing with and without camber and twist

Data presentation of force characteristics of several engine-strut-body configurations at Mach numbers of 1.8 and 2.0 / Robert T. Madden and Emil J. Kremzier

Effects of altitude on turbojet engine performance

Base pressures measured on several parabolic-arc bodies of revolution in free flight at Mach numbers from 0.8 to 1.4 and at large Reynolds numbers

Basic pressure measurements on a fuselage and a 45 degrees sweptback wing-fuselage combination at transonic speeds in the slotted test section of the Langley 8-foot high-speed tunnel

Aerodynamic characteristics of the NACA RM-10 research missile in the Ames 1- by 3-foot supersonic wind tunnel no. 2: Pressure and force measurements at Mach numbers of 1.52 and 1.98

Wind-tunnel tests of a 1/12-scale model of the X-3 airplane at subsonic and supersonic speeds.

Comparison of drag, pressure recovery, and surface pressure of a scoop-type inlet and an NACA submerged inlet at transonic speeds

A specially constructed metallograph for use at elevated temperatures

Relation of engine turbine-blade life to stress-rupture properties of the alloys, Stellite 21, Hastelloy B, Cast S-816, Forged S-816, X-40, Nimonic 80, Refractory 26, N-155, and Iconel X

A recurrence matrix solution for the dynamic response of aircraft in gusts

Investigation of the liquid fluorine-liquid diborane propellant combination in a 100-pound-thrust rocket engine

Buckling of thin-walled cylinder under axial compression and internal pressure

Variation of the pressure limits of flame propagation with tube diameter for propane-air mixtures

Vaporization rates and heat-transfer coefficients for pure liquid drops

Experimental investigation of typical constant- and variable-area exhaust nozzles and effects on axial-flow turbojet-engine performance


Published Year

Subject

Author

‹‹ previous 1 2 ... 19 20 21 22 23 24 25 ... 143 144 next ››