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The near noise field of static jets and some model studies of devices for noise reduction
Additional Experiments With Flat-Top Wing- Body Combinations at High Supersonic Speeds
Cyclic Engine Test of Cast Vitallium Turbine Buckets - 1
Analytical comparison of turbine-blade cooling systems designed for a turbojet engine operating at supersonic speed and high altitude 2: air-cooling systems
Summary Report on Analytical Evaluation of Air and Fuel Specific-Impulse Characteristics of Several Nonhydrocarbon Jet-Engine Fuels
Some Effects of Aeroelasticity at Mach Numbers From 0.7 to 1.6 on the Rolling Effectiveness of Thin Flat-Plate Delta Wings Having 45 Degree Swept Leading Edges and Full-Span Constant-Chord Ailerons
Investigation of thrust and drag characteristics of a plug-type exhaust nozzle
Reciprocity relations in aerodynamics
The Effects of a Highly Cambered Low-Drag Wing and of Auxiliary Flaps on the High-Speed Aerodynamic Characteristics of a Twin-Engine Pursuit Airplane Model
Effects of conical camber on the lift, drag, and pitching-moment characteristics of a triangular wing of aspect ratio 3.0
Two-dimensional transonic investigation of flows and forces on a 9-percent-thick airfoil with 30-percent-chord flap
Comparison of the Combustion Performance of Shell UMF, Grade C, MIL-F-5624C, Grade JP-5, Fuels in a Heavy-Duty XRJ47-W-9 Ram-Jet Engine
Flight Performance of a Twin-Engine Supersonic Ram Jet From 2,300 to 67,200 Feet Altitude
Study of Some Dielectric Properties of Suspensions of Magnesium Particles in Mineral Oil
Experimental Investigation of a Method of Wave-Drag Reduction for Combinations Employing Quasicylindrical Bodies and Swept Wings at Supersonic Speeds
An analog computer study of several stability augmentation schemes designed to alleviate roll-induced instability
A simplified application of the method of operators to the calculation of disturbed motions of an airplane
The effect of nozzle design and operating conditions on the atomization and distribution of fuel sprays
Method and Graphs for the Evaluation of Air-Induction Systems
Investigation of the Effects of Leading-Edge Chord-Extensions and Fences in Combination with Leading-Edge Flaps on the Aerodynamic Characteristics at Mach Numbers from 0.40 to 0.93 of a 45 Degree Sweptback Wing of Aspect Ratio 4
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