Static stability and control of hypersonic gliders
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Rainey, Robert W↗
Engineering topics
Rainey, Robert W
Publications and source records attributed to Rainey, Robert W.
Some Data on Body and Jet Reaction Controls
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Henning, Allen B↗
Investigation at Supersonic Speeds of the Effects of Bomb-bay Configuration upon the Aerodynamic Characteristics of Fuselages with Noncircular Cross Sections
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Rainey, Robert W↗
Wind-tunnel investigation of two vertical-takeoff-and-landing jet bomber airplane configurations at Mach numbers of 1.94 and 2.40
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Jones, Robert A↗
The Effects upon Body Drag of Jets Exhausting from Wing-mounted Nacelles
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Rainey, Robert W↗
Investigation of the Effects of Bomb-bay Configuration upon the Aerodynamic Characteristics of a Body with Circular Cross Section at Supersonic Speeds
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Rainey, Robert W↗
A Wind-tunnel Investigation of Bomb Release at a Mach Number of 1.62
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Rainey, Robert W↗
Effect of Variations in Reynolds Number on the Aerodynamic Characteristics of Three Bomb or Store Shapes at a Mach Number of 1.62 with and Without Fins
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Rainey, Robert W↗
An Investigation of Several Supersonic Missile Configurations Directed Toward Minimizing Center-of-pressure Travel
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Rainey, Robert W↗
Langley 9-inch Supersonic Tunnel Tests of Several Modifications of a Supersonic Missile Having Tandem Cruciform Lifting Surfaces : Three-component Data Results of Models Having Ratios of Wing Span to Tail Span Equal to and Less than 1 and Some Static
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Rainey, Robert W↗
Langley 9-inch Supersonic Tunnel Tests of Several Modifications of a Supersonic Missile Having Tandem Cruciform Lifting Surfaces : Three-component Data Results of Models Having Ratios of Wing Span to Tail Span Equal to 1
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Rainey, Robert W↗
Langley 9-inch supersonic tunnel tests of several modifications of a supersonic missile having tandem cruciform lifting surfaces : three-component data results of models having ratios of wing span to tail span less than 1
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Rainey, Robert W↗
Pressure Measurements at Supersonic Speeds on a Section of a Rectangular Wing Having an NACA 65-009 Profile
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Rainey, Robert W↗
Hinge-moment measurements of a wing with leading-edge and trailing-edge flaps at a Mach number of 1.93
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Rainey, Robert W↗