Browse TRAIL Inventories

Effects of spanwise location of sweep discontinuity on the low-speed static lateral stability characteristics of a complete model with wings of M and W plan form

A method for evaluating the loads and controllability aspects of the pitch-up problem

Application of non-afterburning turbojets to supersonic flight

Application of statistical theory to beam-rider guidance in the presence of noise 1: Wiener filter theory

Application of wing-body theory to drag reduction at low supersonic speeds

Investigation of some wake vortex characteristics of an inclined ogive-cylinder body at Mach number 2

Investigation of some wake vortex characteristics of an inclined ogive-cylinder body at Mach number 1.98

Wind-tunnel investigation at Mach 1.9 of multijet-missile base pressures

Performance of four experimental high btu-per-gallon fuels in a single turbojet combustor

Performance of a supersonic compressor with swept and tilted diffuser blades

Matching of auxiliary inlets to secondary-air requirements of aircraft ejector exhaust nozzles

Some design implications of the effects of aerodynamic heating

Spark ignition of flowing gases 5: application of fuel-air-ratio and initial-temperature data to ignition theory

A special method for finding body distortions that reduce the wave drag of wing and body combinations at supersonic speeds

Panel-flutter investigation at supersonic speeds of a pressurized structure fabricated of 0.020-inch-thick laminated glass-plastic

Analysis of factors affecting selection and design of air-cooled single-stage turbines for turbojet engines 4: coolant-flow requirements and performance of engines using air-cooled corrugated-insert blades

Analytical comparison of convection-cooled turbine blade cooling-air requirements for several radial gas-temperature profiles

Wind-tunnel investigation at low speed of a wing having 63 degree sweepback and a drooped tip

Performance characteristics of axisymmetric two-cone and isentropic nose inlets at Mach number 1.90

A variable-geometry axisymmetric supersonic inlet with telescoping centerbody

Downwash survey behind two low-aspect-ratio variable-incidence wings in combination with three different size fuselages at a Mach number of 0.25

Theoretical analysis of the longitudinal behavior of an automatically controlled supersonic interceptor during the attack phase

Effect of leading-edge sweepback on lift, drag, and pitching-moment characteristics of thin wings of aspect ratio 3 and taper ratio 0.4 at subsonic and supersonic speeds

A study of conical camber for triangular and sweptback wings

Investigation of effectiveness of large-chord slotted flaps in deflecting propeller slipstreams downward for vertical take-off and low-speed flight

Analysis of Low-Temperature Nuclear-Powered Ram-Jet Missile for High Altitudes

Lift, drag, and longitudinal stability at Mach numbers from 1.4 to 2.3 of a rocket-powered model having a 52.5 degree sweptback wing of aspect ratio 3 and inline tail surfaces

Transportation of liquid fluorine

Model investigation of the effect of mounting hydro-skis on shock absorbers

Lift, drag, and longitudinal stability at Mach numbers from 0.8 to 2.1 of a rocket-powered model having a tapered unswept wing of aspect ratio 3 and inline tail surfaces

Performance characteristics of hemispherical target-type thrust reversers

Performance of YJ73-GE-3 turbojet engine in altitude test chamber

Investigation at high subsonic speeds of the effects of various underwing external-store arrangements on the aerodynamic characteristics of a 1/16-scale model of the Douglas D-558-II Research Airplane

An investigation at high subsonic speeds of the effects of horizontal-tail height on the aerodynamic and loading characteristics in sideslip on a 45 degree sweptback, untapered tail assembly as determined from force tests and integrated vertical-tail span loadings

The effect of fluid injection on the compressible turbulent boundary layer : preliminary tests on transpiration cooling of a flat plate

Effect of fuselage fences on the angle-of-attack supersonic performance of a top-inlet-fuselage configuration

A theoretical analysis of the effect of engine angular momentum on longitudinal and directional stability in steady rolling maneuvers

An experimental investigation of the unsteady lift induced on a wing in the downwash field of an oscillating canard control surface

Gust-load and airspeed data from one type of four-engine airplane on five routes from 1947 to 1954

Free-flight investigation to determine some effects of tail damping and wing-tail interference on the rolling effectiveness of inboard and outboard ailerons on an untapered sweptback wing

Free-flight investigation, including some effects of wing aeroelasticity, of the rolling effectiveness of an all-movable horizontal tail with differential incidence at Mach numbers from 0.6 to 1.5

Effects of leading-edge radius on the longitudinal stability of two 45 degree sweptback wings as influenced by Reynolds numbers up to 8.20 x 10(exp 6) and Mach numbers up to 0.303

Development of a new flutter testing technique using a towed dynamic airplane model equipped with an automatic stabilizing system: Experimental and calculated dynamic stability characteristics for speeds up to 200 mph

A survey of unclassified axial-flow-compressor literature

Flight measurements of the vertical-tail loads on the Convair XF-92A delta-wing airplane

Effects of sweep and taper on the longitudinal characteristics of an aspect ratio 3 wing-body combination at Mach numbers from 0.6 to 1.4

A method for simulating the atmospheric entry of long-range ballistic missiles

Flight Determination of the Longitudinal Stability and Control Characteristics of a 0.125-Scale Rocket-Boosted Model of the Mcdonnell F-101 Airplane at Mach Numbers from 0.82 to 1.84

An investigation of string support interference on base pressure and forebody chord force at Mach numbers from 0.60 to 1.30

Collection and summary of flap-type-aileron rolling-effectiveness data at zero lift as determined by rocket-powered model tests at Mach numbers between 0.6 and 1.6


Published Year

Subject

Author

‹‹ previous 1 2 ... 85 86 87 88 89 90 91 ... 143 144 next ››