Study by NACA Wing-flow Method of Transonic Drag Characteristics of a Blunt-nose Body of Revolution and Comparison with Results for a Sharp-nose Body
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Johnston, J Ford↗
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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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The Effects of Compressibility on the Pressures on a Body of Revolution and on the Aerodynamic Characteristics of a Wing-nacelle Combination Consisting of the Body of Revolution Mounted on a Swept-back Wing
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Boltz, Frederick W↗
Preliminary Data on the Effect of Body-nose Bluntness on the Drag and Pressure Recovery of a Side-inlet-body Combination at Mach Numbers of 1.4 and 1.7
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Stroud, John F↗
Experimental and Theoretical Study of the Effects of Body Size on the Aerodynamic Characteristics of an Aspect Ratio 3.0 Wing-body Combination
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Hopkins, Edward J↗
Aerodynamics of Slender Bodies at Mach Number of 3.12 and Reynolds Numbers from 2 x 10(exp 6) to 15 x 10(exp 6) II : Aerodynamic Load Distributions of Series of Five Bodies Having Conical Noses and Cylindrical Afterbodies
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Jack, John R↗
Investigation at High Subsonic Speeds of Bodies Mounted from the Wing of an Unswept-wing-fuselage Model, Including Measurements of Body Loads
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Silvers, H Norman↗
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↗
Aerodynamics of Slender Bodies at Mach Number of 3.12 and Reynolds Numbers from 2 x 10(exp 6) to 15 x 10(exp 6) III : Boundary Layer and Force Measurements on a Slender Cone-cylinder Body of Revolution
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Jack, John R↗
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↗
Free-fall Measurements of the Effects of Wing-body Interference on the Transonic Drag Characteristics of Swept-wing-slender-body Configurations
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Kurbjun, Max C↗
Measurements of fluctuating pressures on the wings and body of a sweptback wing-body combination in the Langley 16-foot transonic tunnel
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Habel, Louis W↗
Preliminary Investigation of the Effects of Body Contouring as Specified by the Transonic Area Rule on the Aerodynamic Characteristics of a Delta Wing-body Combination at Mach Numbers of 1.41 and 2.01
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Carlson, Harry W↗
An investigation of the transonic area rule by flight tests of a sweptback wing on a cylindrical body with and without body indentation between Mach numbers 0.9 and 1.8
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Hoffman, Sherwood↗
Wind-tunnel investigation at low speed of the effect of varying the ratio of body diameter to wing span from 0.1 to 0.8 on the aerodynamic characteristics in pitch of a 45 degree sweptback-wing-body combination
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Johnson, Harold S↗
A transonic wind-tunnel investigation of the effects of twist and camber with and without incidence, twist and body indentation on the aerodynamic characteristics of a 45 degree sweptback wing-body configuration
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Cooper, J Lawrence↗
Transonic wind-tunnel investigation of the effect of body indentation for boattail and cylindrical afterbody shapes on the aerodynamic characteristics of an unswept-wing-body combination
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Kelly, Thomas, C↗