Browse TRAIL Inventories

Stability of bodies of revolution having fineness ratios smaller than 1.0 and having rounded fronts and blunt bases

Air-flow and thrust characteristics of several cylindrical cooling-air ejectors with a primary to secondary temperature ratio of 1.0

Influence of end plates on lift and flow field of a canard-type control surface at a Mach number of 2.00

Hinge-moment characteristics for several tip controls on a 60 degree sweptback delta wing at Mach number 1.61

Effect of inlet oxygen concentration on combustion efficiency of J33 single combustor operating with gaseous propane

Force and pressure recovery characteristics at supersonic speeds of a conical spike inlet with bypasses discharging in an axial direction

Force and pressure recovery characteristics at supersonic speeds of a conical spike inlet with a bypass discharging from the top or bottom of the diffuser in an axial direction

Forced-convection heat-transfer characteristics of molten sodium hydroxide

Altitude wind tunnel investigation of the prototype J40-WE-8 turbojet engine without afterburner

Considerations in the adaptation of low-cost fuels to gas-turbine-powered commercial aircraft

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) III : boundary layer and force measurements on a slender cone-cylinder body of revolution

Acceleration of high-pressure-ratio single-spool turbojet engine as determined from component performance characteristics : effect of compressor interstage air bleed

Experimental investigation of an axial-flow supersonic compressor having rounded leading-edge blades with an 8-percent mean thickness-chord ratio

Experimental investigation of an axial-flow compressor inlet stage operating at transonic relative inlet Mach numbers III : blade-row performance of stage with transonic rotor and subsonic stator at corrected tip speeds of 800 and 1000 feet per secon

Investigation at a Mach number of 1.90 of a diverter-type boundary-layer removal system for a scoop inlet

De-icing and runback characteristics of three cyclic electric, external de-icing boots employing chordwise shedding

A method for calculating the aerodynamic loading on wing-tip-tank combinations in subsonic flow

Investigation at Mach numbers 1.5 and 1.7 of twin-duct side air-intake system with 9 degree compression ramp including modifications to boundary-layer-removal wedges and effects of a bypass system

Preliminary investigation of the effect of fences and balancing tabs on the hinge-moment characteristics of a tip control on a 60 degree delta wing at Mach number 1.61

Preliminary investigation of the effects of body contouring as specified by the transonic area rule on the aerodynamic characteristics of a delta wing-body combination at Mach numbers of 1.41 and 2.01

The low-speed lift and pitching moment characteristics of a 45 degree sweptback wing of aspect ratio 8 with and without high-lift and stall-control devices as determined from pressure distribution at a Reynolds number of 4.0 x 10(exp 6)

A study of the motion and aerodynamic heating of ballistic missiles entering the earth's atmosphere at high supersonic speeds

Some effects of frequency on the contribution of a vertical tail to the free aerodynamic damping of a model oscillating in yaw

Analytical comparison of turbine-blade cooling systems designed for a turbojet engine operating at supersonic speed and high altitude II : air-cooling systems

Analytical comparison of turbine-blade cooling systems designed for a turbojet engine operating at supersonic speed and high altitude I : liquid-cooling systems

An analysis of the tracking performances of two straight-wing and two swept-wing fighter airplanes with fixed sights in a standardized test maneuver

Analysis of the turbojet engine for propulsion of supersonic fighter airplanes

Analysis of turbine stator adjustment required for compressor design-point operation in high Mach number supersonic turbojet engines

Wing loads on the Bell X-1 research airplane (10 percent thick wing) as determined by pressure-distribution measurements in flight at subsonic and transonic speeds

Wind-tunnel investigation of the behavior of parachutes in close proximity to one another

Wind-tunnel investigation of the vortex wake and downwash field behind triangular wings and wing-body combinations at supersonic speeds

Aerodynamic characteristics at high and low subsonic Mach numbers of four NACA 6-series airfoil sections at angles of attack from -2 to 31 degrees

An experimental investigation at subsonic and supersonic speeds of the torsional damping characteristics of a constant-chord control surface of an aspect ratio 2 triangular wing

Experimental investigation of a 0.4 hub-tip diameter ratio axial-flow compressor inlet stage at transonic inlet relative Mach numbers I : rotor design and over-all performance at tip speeds from 60 to 100 percent of design

Effects of rate of flap deflection on flap hinge moment and wing lift through the Mach number range from 0.32 to 0.87

Free-flight performance of a rocket-boosted, air-launched 16-inch-diameter ram-jet engine at Mach numbers up to 2.20

Free-flight tests of three 1/9-scale models of the wing-ram-jet configuration of the Grumman XSSM-N-6A (Rigel) missile to investigate the possibility of flutter : TED No. NACA DE 223

Free-flight-tunnel investigation of the low-speed stability and control characteristics of a canard airplane model

Free-flight longitudinal-stability investigation including some effects of wing elasticity from Mach numbers of 0.85 to 1.34 of a tailless missile configuration having a 45 degree sweptback wing of aspect ratio 5.5

Ignition delays of some nonaromatic fuels with low-freezing red fuming nitric acid in temperature range -40 to -105 degrees F

Internal performance characteristics of variable-throat plug- and vaned-type convergent-divergent nozzles

Effect of axially staged fuel introduction on performance of one-quarter sector of annular turbojet combustor

Comparison of pressure-loss characteristics of several tail-cone air-induction systems for air-cooled gas-turbine rotors

The effects of fences on the high-speed longitudinal stability of a swept-wing airplane

Comparison of the aerodynamic characteristics at transonic speeds of a plane wing and a cambered and twisted wing, both having 45 degrees of sweepback and an aspect ratio of 6

Comparison of theoretical and experimental zero-lift drag-rise characteristics of wing-body-tail combinations near the speed of sound

Effect of leading-edge chord-extensions on the aerodynamic characteristics of a 45 degree sweptback wing-fuselage combination at Mach numbers of 0.40 to 1.03

Effect of leading-edge chord-extensions on subsonic and transonic aerodynamic characteristics of three models having 45 degrees sweptback wings of aspect ratio 4

Effects of slot location and geometry on the flow in a square tunnel at transonic Mach numbers

Effects of slot size and geometry on the flow in rectangular tunnels at Mach numbers up to 1.4


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