Lift and moment responses to penetration of sharp-edged traveling gusts, with application to penetration of weak blast waves
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Drischler, Joseph A↗
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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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Study of Pressure Distributions on Simple Sharp-nosed Models at Mach Numbers from 16 to 18 in Helium Flow
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Erickson, Wayne D↗
Flight tests at transonic and supersonic speeds of an airplane-like configuration with thin straight sharp-edge wings and tail surfaces
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Mitchell, Jesse L↗
An Investigation of the Low-speed Characteristics of Two Sharp-edge Supersonic Inlets Designed for Essentially External Supersonic Compression
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Dennard, John S↗
Aerodynamic characteristics at subcritical and supercritical Mach numbers of two airfoil sections having sharp leading edges and extreme rearward positions of maximum thickness
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Eggers, A J , Jr↗
Pressure Distribution over a Sharp-nose Body of Revolution at Transonic Speeds by the NACA Wing-flow Method
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Danforth, Edward C B↗
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↗
Error in airspeed measurement due to static-pressure field ahead of sharp-nose bodies of revolution at transonic speeds
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Danforth, Edward C↗
The Aerodynamic Characteristics Throughout the Subsonic Speed Range of a Thin, Sharp-edged Horizontal Tail of Aspect Ratio 4 Equipped with a Constant-chord Elevator
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Bandettini, Angelo↗
Flight Investigation of the Effect of Thickening the Aileron Trailing Edge on Control Effectiveness for Sweptback Tapered Wings Having Sharp-and Round-nose Sections
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Strass, H Kurt↗
A method for predicting the low speed chordwise pressure distribution over sharp edge airfoil sections with plain flaps at the leading and trailing edges
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Nuber, Robert J↗
A low-speed experimental study of the directional characteristics of a sharp-nosed fuselage through a large angle-of-attack range at zero angle of sideslip
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Letko, William↗
Application of transonic area rule to a sharp-lipped ducted nacelle
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Walters, Richard E↗
Some internal-flow characteristics at zero flight speed of an annular supersonic inlet and an open-nose inlet with sharp and rounded lips
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Milillo, Joseph R↗
Experimental investigation of an axial-flow supersonic compressor having sharp leading-edge blades with an 8-percent mean thickness chord ratio
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Goldberg, Theodore J↗
Low-speed Lateral-control Characteristics of an Unswept Wing with Hexagonal Airfoil Sections and Aspect Ratio 2.5 Equipped with Spoilers and with Sharp- and Thickened-trailing-edge Flap-type Ailerons at a Reynolds Number of 7.6 x 10(exp 6)
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Fitzpatrick, James E↗
Comparison at Supersonic Speeds of Translating Spike Inlets Having Blunt- and Sharp-lip Cowls
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Gorton, Gerald, C↗
A flat wing with sharp edges in a supersonic stream
A basic treatment is given for the approximate solution of the problem of two-dimensional supersonic flow past a thin wing at small angles of attack. The pressure distribution at the surface, the lifting force, and the wave drag are determined.
AERODYNAMICS, FUNDAMENTAL↗