Wind-tunnel Investigation of the Effects of a Jet Engine Nacelle on the Aerodynamic Characteristics of a 37.25 Degree Swept Back Wing at High Subsonic Speeds
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Boltz, Federick W↗
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Results for “TUNNEL EFFECT”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Wind-tunnel Investigation of the Effects of Various Asymmetric Canopy Modifications on the Behavior of Descending Parachutes
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Scher, Stanley H↗
Full-scale Wind-tunnel Investigation of the Effects of Wing Modifications and Horizontal-tail Location on the Low-speed Static Longitudinal Characteristics of a 35 Degree Swept-wing Airplane
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Maki, Ralph L↗
Low-speed Wind-tunnel Investigation of the Effects of Propeller Operation at High Thrust on the Longitudinal Stability and Trim of a Twin-engine Airplane Configuration
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Sleeman, William C , Jr↗
Transonic wind-tunnel investigation of the effects of wing incidence angle on the characteristics of two wing-body combinations
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Morgan, Francis G , Jr↗
A Transonic Wind-tunnel Investigation of the Effects of Longitudinal Wing Location and Varying Body Size on the Interference Characteristics of a 45 Degrees Sweptback Wing
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Loving, Donald L↗
A Transonic Wind-tunnel Investigation of the Effects of Body Indentation, as Specified by the Transonic Drag-rise Rule, on the Aerodynamic Characteristics and Flow Phenomena of a 45 Degree Sweptback-wing-body Combination
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Robinson, Harold L↗
Transonic wind-tunnel investigation of the effects of aspect ratio, spanwise variations in section thickness ratio, and a body indentation on the aerodynamic characteristics of a 45 degree sweptback wing-body combination
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Carmel, Melvin M↗
A Transonic Wind-tunnel Investigation of the Effects of Body Indentation, as Specified by the Transonic Drag-rise Rule, on the Aerodynamic Characteristics and Flow Phenomena of an Unswept-wing-body Combination
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Williams, Claude V↗
Gust-tunnel Investigation to Determine Effects of Center-of-gravity Position on the Gust Loads of a Delta-wing Model with Leading Edge Swept Back 60 Degrees
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Reisert, Thomas D↗
Plate Method of Ground Representation for Wind-tunnel Determination of Elevator Effectiveness in Landing
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Recant, I G↗
Wind-tunnel Investigation of the Effect of Vertical Position of the Wing on the Side Flow in the Region of the Vertical Tail
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Recant, Isidore G↗
A Transonic Wind-tunnel Investigation of the Effect of Modifications to an Indented Body in Combination with a 45 Degree Sweptback Wing
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Loving, Donald L↗
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
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Kuhn, Richard E↗
A transonic wind-tunnel investigation of the effects of body indentation on the aerodynamic characteristics of an approximate-delta-wing-body configuration, and a comparison with a wing of reversed plan form
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Williams, Claude V↗
Wind-tunnel Investigation of the Effects of Geometric Dihedral on the Aerodynamic Characteristics in Pitch and Sideslip of an Unswept- and a 45 Degree Sweptback-wing-fuselage Combination at High Subsonic Speeds
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Kuhn, Richard E↗
A transonic wind-tunnel investigation of the effects of nacelles on the aerodynamic characteristics of a complete model configuration
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Carmel, Melvin M↗
Wind-tunnel investigation of the effects of various dorsal-fin and vertical-tail configurations on the directional stability of a streamlined body at transonic speeds : transonic-bump method
Yawing-moment coefficients were obtained for several dorsal-fin and vertical-tail configurations in combination with a streamlined body through a large angle-of-sideslip range and a Mach number range of 0.59 to 1.11. The results indicated that dorsal fins improved the directional stability characteristics of the body alone and the body-vertical-tail configuration. A ring tail was more effective at small angles of sideslip and less effective at large angles of sideslip than a tapered low-aspect-ratio vertical tail.
TAIL-BODY COMBINATIONS - MISSILES↗