TRAIL - Technical Report Archive and Image Library

Low-speed experimental investigation of the magnus effect on various sections of a body of revolution with and without a propeller

Measurement of static pressure on aircraft

Measurement of aerodynamic forces for various mean angles of attack on an airfoil oscillating in pitch and on two finite-span wings oscillating in bending with emphasis on damping in the stall

The measurement of pressure altitude on aircraft

Exploratory study of ground proximity effects on thrust of annular and circular nozzles

Results of the flight test of a 0.13-scale rocket-boosted model of the McDonnell F4H-1 airplane between Mach numbers of 0.20 and 1.90: TED No. NACA AD 3115

Flight tests of an automatic interceptor system with a tracking radar modified to minimize the interaction between antenna and interceptor motions

Exploratory investigation of aerodynamic effects of external combustion of aluminum borohydride in airstream adjacent to flat plate in Mach 2.46 tunnel

Full-scale free-jet investigation of a two-shock side-inlet diffuser at Mach 2.75 and a comparison with a single-shock diffuser

Impact-loads investigation of chine-immersed models having concave-convex transverse shape and straight or curved keel lines

Impact-loads investigation of a chine-immersed model having a longitudinally curved bow and a v-bottom with a dead-rise angle of 30 degrees

Heat transfer and boundary-layer transition on two blunt bodies at Mach numbers 3.12

Heat transfer and recovery temperatures on a sphere with laminar, transitional, and turbulent boundary layers at Mach numbers of 2.00 and 4.15

Heat-exchanger-core weights for use with hydrogen expansion turbine

A note on the effect of heat transfer on peak pressure rise associated with separation of turbulent boundary layer on a body of revolution (NACA RM-10) at a Mach number of 1.61

Investigation of a nonlinear control system

Preliminary investigation of the characteristics of a two dimensional wing and propeller with the propeller plane of rotation in the wing-chord plane

Investigation of a nonlinear control system

Recent research on the creep of airframe components

Applications of power spectral analysis methods to maneuver loads obtained on jet fighter airplanes during service operations

Effect of fiber orientation on ball failures under rolling-contact conditions

Effect of crystal orientation on fatigue-crack initiation in polycrystalline aluminum alloys

Arrangements of jet engine and airframe for increased range

Effect of fuel properties on liner temperatures in a single tubular turbojet combustor

Creep behavior of structural joints of aircraft materials under constant loads and temperatures

Creep deformation patterns of joints under bearing and tensile loads

Drop burning rates of hydrocarbon and nonhydrocarbon fuels

Effect of lubricant viscosity on rolling-contact fatigue life

Effect of nose shape on subsonic aerodynamic characteristics of a body of revolution having a fineness ratio of 10.94

Effect of overheating on creep-rupture properties of HS-31 alloy at 1,500 F

Analytical investigation of the effect of water injection on supersonic turbojet-engine - inlet matching and thrust augmentation

Analytical study of the comparative pitch-up behavior of several airplanes and correlation with pilot opinion

Calculated and measured stresses in simple panels subject to intense random acoustic loading including the near noise field of a turbojet engine

Cascade investigation of cooling characteristics of a cast-finned air-cooled turbine blade for use in a turboprop engine

A comparison of carrier approach speeds as determined from flight tests and from pilot-operated simulator studies

Comparison of calculated and experimental load distributions on thin wings at high subsonic and sonic speeds

Comparison of effect of a turbojet engine and three cold-flow configurations on the stability of a full-scale supersonicle inlet

Combustor performance of a 16-inch ram jet using gaseous hydrogen as fuel at Mach number 3.0

An analytical investigation of the gust-alleviating properties of a simple pitch damper

Analysis of operational airline data to show the effects of airborne weather radar on the gust loads and operating practices of twin-engine short-haul transport airplanes

Flight tests of a model of a high-wing transport vertical-take-off airplane with tilting wing and propellers and with jet controls at the rear of the fuselage for pitch and yaw control

Comparison of NACA 65-series compressor-blade pressure distributions and performance in a rotor and in cascade

Analysis of experimental low-speed loss and stall characteristics of two-dimensional compressor blade cascades

Analysis of fluorine addition to the vanguard first stage

Analysis of horizontal-tail loads in pitching maneuvers on a flexible swept-wing jet bomber

Characteristics of a 40 degree cone for measuring Mach number, total pressure, and flow angles at supersonic speeds

The combinations of thermal and load stresses for the onset of permanent buckling in plates

Comparison of experimental with theoretical total-pressure loss in parallel-walled turbojet combustors

Component performance investigation of J71 experimental turbine VII: effect of first-stator adjustment; over-all performance of J71 turbine with 87-percent-design stator area

Compressible laminar boundary layer over a yawed infinite cylinder with heat transfer and arbitrary Prandtl number

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