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Spontaneous ignition temperatures of pure hydrocarbons and commercial fluids
Effective Modulus in Plastic Buckling of High-Strength Aluminum-Alloy Sheet
A two-dimensional cascade study of the aerodynamic characteristics of a turbine-rotor blade suitable for air cooling
Review of Current and Anticipated Lubricant Problems in Turbojet Engines
Longitudinal Stability, Control Effectiveness, and Drag Characteristics at Transonic Speeds of a Rocket-Propelled Model of an Airplane Configuration Having an Unswept Tapered Wing of Aspect Ratio 3.0 and NACA 65A004.5 Airfoil Sections
The low-speed lift and pitching moment characteristics of a 45 degree sweptback wing of aspect ratio 8 with and without high-lift and stall-control devices as determined from pressure distribution at a Reynolds number of 4.0 x 10(exp 6)
Investigation at Transonic Speeds of the Effect of a Positive-Lift Balancing Tab on the Hinge-Moment and Lift-Characteristics of a Full-Span Flap on a Tapered 45 Degrees Sweptback Wing of Aspect Ratio 3
Performance of a supersonic mixed-flow rotor with a swept leading edge and 0.52 inlet radius ratio
Exploratory engine test of transpiration-cooled turbine-rotor blade with wire-cloth shell
Low-speed lateral control characteristics of an unswept wing with hexagonal airfoil sections and aspect ratio 4.0 at a Reynolds number of 6.2 x 10(exp 6)
Results of measurements of maximum lift and buffeting intensities obtained during flight investigation of the Northrop X-4 research airplane
Friction and surface damage of several corrosion-resistant materials
Theoretical performance of liquid ammonia, hydrazine and mixture of liquid ammonia and hydrazine as fuels with liquid oxygen biflouride as oxidant for rocket engines 1: mixture of liquid ammonia and hydrazine
Some Measurements of Buffeting Encountered by Douglas D-558-II Research Airplane in the Mach Number Range From 0.5 to 0.95
Large-scale flight measurements of zero-lift drag and low-lift longitudinal characteristics of a diamond-wing-body combination at Mach numbers from 0.725 to 1.54
Low-Speed Investigation of the Aerodynamic, Control, and Hinge-Moment Characteristics of Two Types of Controls on a Delta-Wing-Fuselage Model With and Without Nacelles
Wind-Tunnel Investigation of the Effects of a Fence and a Leading-Edge Notch on the Aerodynamic Loading Characteristics in Pitch of a 45 Degree Sweptback Wing at High Subsonic Speeds
Analysis of performance of four symmetrical-diagram-type subsonic inlet-stage axial-flow compressors
Flight Determination of the Static Longitudinal Stability Boundaries of the Bell X-5 Research Airplane with 59 Degrees Sweepback
Investigation of the Effects of Leading-Edge Flaps on the Aerodynamic Characteristics in Pitch at Mach Numbers From 0.40 to 0.93 of a Wing-Fuselage Configuration With a 45 Degree Sweptback Wing of Aspect Ratio 4
Effect of a leading-edge flap upon the lift, drag, and pitching moment of an airplane employing a thin, unswept wing
Aerodynamic control of supersonic inlets for optimum performance
Investigation of a Flow Deflector and an Auxiliary Scoop for Improving Off-Design Performance of Nose Inlets
Transonic Longitudinal Aerodynamic Effects of Sweeping Up the Rear of the Fuselage of a Rocket-Propelled Airplane Model Having No Horizontal Tail
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