Search results for: Covell, Peter F.
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1
Effects of axisymmetric and normal air jet plumes and solid plume on cylindrical afterbody pressure distributions at Mach numbers from 1.65 to 2.50
Authors: Covell, Peter F.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1982Physical Description: 32 pages : illustrations ; 28 cm.Holdings: Loading…
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2
Investigation of leading-edge flap performance on delta and double-delta wings at supersonic speeds
Authors: Covell, Peter F.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1987Physical Description: 1 volume.Holdings: Loading…
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3
Longitudinal and lateral-directional aerodynamic characteristics of a wing-cone configuration at Mach numbers from 2.5 to 4.5
Authors: Covell, Peter F.
Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [For sale by the National Technical Information Service], 1992Physical Description: 1 volume.Holdings: Loading…
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4
Interference effects of aft reaction-control yaw jets on the aerodynamic characteristics of a space shuttle orbiter model at supersonic speeds
Authors: Covell, Peter F.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1983Physical Description: 44 pages : illustrations ; 28 cm.Holdings: Loading…
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5
Experimental and theoretical study of longitudinal aerodynamic characteristics of delta and double-delta wings at Mach numbers of 1.60, 1.90, and 2.16
Authors: Wood, Richard M., Covell, Peter F.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985Physical Description: 1 online resource (119 pages) : illustrations.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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6
Experimental and theoretical study of the longitudinal aerodynamic characteristics of delta and double-delta wings at mach numbers of 1.60, 1.90, and 2.16
Authors: Wood, Richard M., Covell, Peter F.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985Physical Description: 1 online resource (119 pages, 1 unnumbered page) : illustrations.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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7
Effects of winglets on a first-generation jet transport wing : VII, sideslip effects on winglet loads and selected wing loads at subsonic speeds for a full-span model
Authors: Meyer, Robert R.Other Authors: “…Covell, Peter F.…”
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1986
Physical Description: 1 volume.Holdings: Loading…
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8
Aerodynamic characteristics of a series of bodies with variations in nose camber
Authors: Shrout, Barrett L.Other Authors: “…Covell, Peter F.…”
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1983
Physical Description: 52 pages : illustrations ; 28 cm.Holdings: Loading…
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9
Experimental and theoretical study of the longitudinal aerodynamic characteristics of delta and double-delta wings at mach numbers of 1.60, 1.90, and 2.16
Authors: Wood, Richard M.Other Authors: “…Covell, Peter F.…”
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; For sale by the National Technical Information Service, 1985
Physical Description: 1 volume.Holdings: Loading…
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10
Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0
Authors: Walker, Ira J.Other Authors: “…Covell, Peter F.…”
Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [National Technical Information Service, distributor], 1993
Physical Description: 1 volume.Holdings: Loading…
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Related Subjects
Delta wings
Aerodynamics, Supersonic
Mach number
Supersonic airfoils
Supersonic flow
Aerodynamics
Airplanes
Sweptback wings
Aerodynamic characteristics
Aerodynamic drag
Canard configurations
Cone
Delta wing airplanes
Drag (Aerodynamics)
Hypersonic vehicles
Hypersonics
Interference (Aerodynamics)
Noses (Aircraft)
Research vehicles
Space shuttles
Stabilizers (Fluid dynamics)
Supersonic wind tunnels
Tail assemblies
Wind tunnel tests
Wings
Wings, Triangular