Browse TRAIL Inventories

Skin-friction measurements in incompressible flow

Analysis of effects of interceptor roll performance and maneuverability on success of collision-course attacks

Boundary-induced downwash due to lift in a two-dimensional slotted wind tunnel

Boundary-layer stability diagrams for electrically conducting fluids in the presence of a magnetic field

Effect of lubricant base stock on rolling-contact fatigue life

Effect of prior air force over temperature operation on life of J47 buckets evaluated in a sea-level cyclic engine test

Effect of wall cooling on inlet parameters of a scoop operating in a turbulent boundary layer on a flat or conical surface for Mach numbers 2 to 10

An evaluation of the effects of flexibility on wing strains in rough air for a large swept-wing airplane by means of experimentally determined frequency-response functions with an assessment of random-process techniques employed

Experimental ablation cooling

Effectiveness of various protective coverings on magnesium fins at Mach number 2.0 and stagnation temperatures up to 3,600 R

Effects of nose and afterbody modifications on aerodynamic characteristics of a body with and without a vertical tail at a Mach number of 2.01

Effects of Mach number and wall-temperature ratio on turbulent heat transfer at Mach numbers from 3 to 5

Effects of modifications to a control surface on a 6-percent-thick unswept wing on the transonic control-surface flutter derivatives

Effect of overheating on creep-rupture properties of M-252 alloy

The effect of moment-of-area-rule modifications on the zero-lift drag of three wing-body combinations

The effects of target and missile characteristics on theoretical minimum miss distance for a beam-rider guidance system in the presence of noise

An estimate of the fluctuating surface pressures encountered in the reentry of a ballistic missile

Experimental behavior of pentaborane-air combustion products during expansion in a convergent-divergent nozzle

An experimental investigation of sting-support effects on drag and a comparison with jet effects at transonic speeds

Experimental investigation of the effect of yaw on rates of heat transfer to transverse circular cylinders in a 6500-foot-per-second hypersonic air stream

Experimental investigation of the drag of flat plates and cylinders in the slipstream of a hovering rotor

An experimental investigation of the effect of various parameters including tip Mach number on the flutter of some model helicopter rotor blades

Experimental investigation of the drag due to wedges along the trailing edge of a swept wing

Aerodynamic characteristics of a 45 degree swept-wing fighter-airplane model and aerodynamic loads on adjacent stores and missiles at Mach numbers of 1.57, 1.87, 2.16, and 2.53

A comparison of two methods for calculating transient temperatures for thick walls

Aerodynamic characteristics of a canard and an outboard-tail airplane model at a Mach number of 2.01

Investigation of Reynolds number effect on performance of an eight-stage axial-flow research compressor with long- and medium-chord lengths in the two transonic inlet stages

Preliminary analysis of over-all performance of an eight-stage axial -flow research compressor with two long-chord transonic inlet stages

Tabulated pressure data for a 60 degree delta-wing-body-tail model with a hot jet exhausting from a pylon-mounted nacelle

Supersonic wave interference affecting stability

Propellant vaporization as a criterion for rocket engine design : relation between percentage of propellant vaporized and engine performance

Similar solutions for the compressible boundary layer on a yawed cylinder with transpiration cooling

Some factors affecting the variation of pitching moment with sideslip of aircraft configurations

Study of exit phase of flight of a very high altitude hypersonic airplane by means of a pilot-controlled analog computer

The static and dynamic-rotary stability derivatives at subsonic speeds of a model of the X-15 research airplane

Results of an experimental investigation of small viscous dampers

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

Static stability and control of canard configurations at Mach numbers from 0.70 to 2.22: triangular wing and canard on an extended body

Static stability and control characteristics of a triangular wing and canard configuration at Mach numbers form 2.58 to 3.53

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


Published Year

Subject

Author

‹‹ previous 1 2 ... 268 269 270 271 272 273 274 ... 280 281 next ››