Search
Search U.S. government technical reports digitized or harvested by TRAIL.
Keyword Search
14045 results returnedSearch results
- 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