Browse TRAIL Inventories

Static stability and control of canard configurations at Mach numbers from 0.70 to 2.22: longitudinal characteristics of an unswept wing and canard

The static longitudinal characteristics of a twisted and cambered 45 degree sweptback wing at Mach numbers up to 0.96

Static stability and control of canard configurations at Mach numbers from 0.70 to 2.22 : longitudinal characteristics of a triangular wing and canard

Static stability and control of canard configurations at Mach numbers from 0.70 to 2.22longitudinal characteristics of a triangular wing and unswept canard

Propellant vaporization as a criterion for rocket-engine design : calculations of chamber length to vaporize various propellants

Survey of supersonic inlets for high Mach number applications

Effects of vertical location of the wing and horizontal tail on the static lateral and directional stability of a trapezoidal-wing airplane model at Mach numbers of 1.41 and 2.01

Experimental measurements of the effects of airplane motions on wing and tail angles of attack of a swept-wing bomber in rough air

Experimental results of an investigation of two methods of inflight thrust measurement applicable to afterburning turbojet engines with ejectors

An experimental investigation of wake effects on hydro-skis

Effect of a stringer on the stress concentration due to a crack in a thin sheet

Effect of a hot-jet exhaust on pressure distributions and external drag of several afterbodies on a single-engine airplane model at transonic speeds

Dynamic stability of vehicles traversing ascending or descending paths through the atmosphere

Effect of aerodynamic heating on the flutter of a rectangular wing at a Mach number of 2

Effects of nose angle and Mach number on transition on cones at supersonic speeds

Effects of frequency and amplitude on the yawing derivatives of triangular, swept, and unswept wings and of a triangular-wing-fuselage combination with and without a triangular tail performing sinusoidal yawing oscillations

Effects of fixing transition on the transonic aerodynamic characteristics of a wing-body configuration at Reynolds numbers from 2.4 to 12 million

Idealized wings and wing-bodies at a Mach number of 3

Flight investigation of the acceptability of a small side-located controller used with an irreversible hydraulic control system

General solutions for flow past slender cambered wings with swept trailing edges and calculation of additional loading due to control surfaces

Free-flight pressure measurements over a flare-stabilized rocket model with a modified Von Karman nose for Mach numbers up to 4.3

Transonic drag of several jet-noise suppressors

Investigation of a 0.6 hub-tip radius-ratio transonic turbine designed for secondary-flow study 4: rotor loss patterns as determined by hot-wire anemometers with rotor operating in a circumferentially uniform inlet flow field

Incipient spin characteristics of a 1/25-scale model of the Chance Vought XF8U-1 airplane: TED No. NACA AD 3118

Induction system characteristics and engine surge occurrence for two fighter-type airplanes

Subsonic aerodynamic characteristics up to extreme angles of attack of an airplane model having an unswept wing and a high horizontal tail

Summary of experimental heat-transfer measurements in turbulent flow for a Mach number range from 0.87 to 5.05

Summary of locations, extents, and intensities of turbulent areas encountered during flight investigations of the jet stream from January 7, 1957 to April 28, 1957

Theoretical combustion performance of several high-energy fuels for ramjet engines

Aerodynamic heating of blunt nose shapes at Mach numbers up to 14

A wind-tunnel investigation of several wingless missile configurations at supersonic speeds

Wind-tunnel investigation of the aerodynamic and structural deflection characteristics of the Goodyear Inflatoplane

Tests of ring-stiffened circular cylinders subjected to a transverse shear load

The adhesion of molten boron oxide to various materials

Aerodynamic characteristics at Mach numbers 2.36 and 2.87 of an airplane configuration having a cambered arrow wing with a 75 degree swept leading edge

Tracking performance of a swept-wing fighter with a director-type radar fire-control system and scope presentation

Torque-speed characteristics for high-specific-work turbines

Investigation of two bluff shapes in axial free flight over a Mach number range from 0.35 and 2.15

Limited investigation of noise suppression by injection of water into exhaust of afterburning jet engine

Limited tests of molybdenum coated with molybdenum disilicide in a supersonic heated-air jet and brief description of the coating facility

Low-subsonic investigation to determine the chordwise pressure distribution and effectiveness of spoilers on a thin, low-aspect-ratio, unswept, untapered, semispan wing and on the wing with leading and trailing-edge flaps

Low tire friction and cornering forces on a wet surface

Aerodynamic Heating of Blunt Nose Shapes at Mach Numbers Up to 14

Preliminary Aerodynamic Data Pertinent to Manned Satellite Reentry Configurations

Preliminary Analysis of a Nuclear Powered Supersonic Airplane Using Ramjet Engines

Preliminary Analysis of Hydrogen-Rich Hypersonic Ramjet Operation

Off-Design Performance of Divergent Ejectors

Performance at Mach Numbers 3.07, 1.89, and 0 of Inlets Designed for Inlet-Engine Matching Up to Mach 3

Performance of Five Short Multielement Turbojet Combustors for Hydrogen Fuel in Quarter-Annulus Duct

A Preliminary Study of the Effect of Boric Oxide Deposits on the Performance of Two Selected Turbine Stator-Blade Shapes


Published Year

Subject

Author

‹‹ previous 1 2 ... 134 135 136 137 138 139 140 ... 143 144 next ››