Effects of Nose and Afterbody Modifications on Aerodynamic Characteristics of a Body with and Without a Vertical Tail at a Mach Number of 2.01
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Foster, Gerald V↗
Engineering topics
Foster, Gerald V
Publications and source records attributed to Foster, Gerald V.
Investigation of the Longitudinal Aerodynamic Characteristics of a Trapezoidal-wing Airplane Model with Various Vertical Positions of Wing and Horizontal Tail at Mach Numbers of 1.41 and 2.01
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Foster, Gerald V↗
A study of several factors affecting the stability contributed by a horizontal tail at various vertical positions on a sweptback-wing airplane model
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Foster, Gerald V↗
Static Longitudinal Stability and Control Characteristics of a Model of a 45 Degree Swept-wing Fighter Airplane at Mach Numbers of 1.41, 1.61, and 2.01
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Driver, Cornelius↗
Effects of leading-edge radius on the longitudinal stability of two 45 degree sweptback wings incorporating leading edge camber as influenced by Reynolds numbers up to 8.00 x 10(exp 6) and Mach numbers up to 0.29
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Foster, Gerald V↗
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
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Foster, Gerald V↗
Longitudinal Stability and Wake-flow Characteristics of a Twisted and Cambered Wing-fuselage Combination of 45 Degree Sweepback and Aspect Ratio 8 with a Horizontal Tail and Stall-control Devices at a Reynolds Number of 4.0 x 10(exp 6).
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Foster, Gerald V↗
Low-speed longitudinal characteristics of an unswept hexagonal wing with and without a fuselage and a horizontal tail located at various positions at Reynolds numbers from 2.8 x 10(exp 6) to 7.6 x 10(exp 6)
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Foster, Gerald V↗
Effects of Twist and Camber, Fences, and Horizontal-tail Height on the Low-speed Longitudinal Stability Characteristics of a Wing-fuselage Combination with a 45 Degree Sweptback Wing of Aspect Ratio 8 at a Reynolds Number of 4.0 x 10(exp 6)
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Foster, Gerald V↗
Low-speed longitudinal and wake air-flow characteristics at a Reynolds number of 5.5 x 10(exp 6) of a circular-arc 52 degrees sweptback wing with a fuselage and a horizontal tail at various vertical positions
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Foster, Gerald V↗
Low-speed longitudinal and wake air-flow characteristics at a Reynolds number of 6.0 x 10(exp 6) of a 52 degree sweptback wing equipped with various spans of leading-edge flaps, a fuselage, and a horizontal tail at various vertical positions
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Griner, Roland F↗
Low-speed longitudinal characteristics of a circular-arc 52 degree sweptback wing of aspect ratio 2.84 with and without leading-edge and trailing-edge flaps at Reynolds numbers from 1.6 x 10(exp 6) to 9.7 x 10(exp 6)
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Foster, Gerald V↗
A study of several factors affecting the stability contributed by a horizontal tail at various vertical positions on a sweptback-wing airplane model
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Foster, Gerald V↗
Longitudinal-stability Investigation of High-lift and Stall-control Devices on a 52 Degree Sweptback Wing with and Without Fuselage and Horizontal Tail at a Reynolds Number of 6.8 x 10(exp 6).
Contains low-speed longitudinal stability characteristics of a 52 degree sweptback wing of aspect ratio 2.88, taper ratio 0.625, and NACA 64 (sub 1)-112 airfoil sections normal to the 0.282-chord line, in combination with split flaps, leading-edge flaps, and upper-surface fences. Low-wing and midwing-fuselage aerodynamic characteristics are presented with and without a horizontal tail at various vertical locations. Tests were conducted at a Reynolds number of 6.8 x 10(exp 6).
STABILITY, LONGITUDINAL - STATIC↗
Static Longitudinal Aerodynamic Characteristics of a 52 Degree Sweptback Wing of Aspect Ratio 2.88 at Reynolds Numbers from 2,000,000 to 11,000,000
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Fitzpatrick, James E↗