Search results for: Stallings, Robert L.
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1
Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3
Authors: Stallings, Robert L.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1980Physical Description: 45 pages : illustrations ; 27 cm.Holdings: Loading…
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2
Effect of Reynolds number on stability characteristics of a cruciform wing-body at supersonic speeds
Authors: Stallings, Robert L.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Office ; [for sale by the National Technical Information Service], 1980Physical Description: 108 unnumbered pages : illustrations ; 27 cm.Holdings: Loading…
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3
Wing-alone aerodynamic characteristics for high angles of attack at supersonic speeds
Authors: Stallings, Robert L.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1981Physical Description: 187 pages : illustrations ; 28 cm.Holdings: Loading…
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4
Experimental cavity pressure distributions at supersonic speeds
Authors: Stallings, Robert L.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1987Physical Description: 1 volume.Holdings: Loading…
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5
Measurements of forces, moments, and pressures on a generic store separating from a box cavity at supersonic speeds
Authors: Stallings, Robert L.
Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [For sale by the National Technical Information Service], 1991Physical Description: 1 volume.Holdings: Loading…
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6
Aerodynamic characteristics of a Sparrow III missile model in the flow field of a generalized parent body at Mach 2.86
Authors: Stallings, Robert L.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1981Physical Description: 26 pages : illustrations ; 28 cm.Holdings: Loading…
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7
Effects of roughness size on the position of boundary-layer transition and on the aerodynamic characteristics of a 55 s̊wept delta wing at supersonic speeds
Authors: Stallings, Robert L.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1977Physical Description: 47 pages : illustrations ; 27 cm.Holdings: Loading…
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8
Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3
Authors: Stallings, Robert L., Lamb, Milton
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980Physical Description: 1 online resource (45 pages) : illustrations.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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9
Analysis of the performance of the drive system and diffuser of the Langley Unitary Plan Wind Tunnel
Authors: Hasel, Lowell E.Other Authors: “…Stallings, Robert L.…”
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1981
Physical Description: 64 pages : illustrations ; 28 cm.Holdings: Loading…
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10
Effect of passive venting on static pressure distributions in cavities at subsonic and transonic speeds
Published: National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1994Other Authors: “…Stallings, Robert L.…”
Physical Description: 1 volume.Holdings: Loading…
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11
Supersonic axial-force characteristics of a rectangular-box cavity with various length-to-depth ratios in a flat plate
Authors: Blair, A. B.Other Authors: “…Stallings, Robert L.…”
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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Related Subjects
Aerodynamics, Supersonic
Boundary layer
Supersonic wind tunnels
Aerothermodynamics
Airplanes
Cavities (Airplanes)
Flow distribution
Wind tunnel tests
Wings
Aerodynamic load
Aircraft structures
Boundary layer flow
Boundary layer stability
Cavitation flow
Cavities
Countermeasures
Drag (Aerodynamics)
Drag reduction
Flat plates
Flow visualization
Guided missiles
Heat transfer
Pressure distribution
Reynolds number
Stability of airplanes
Static pressure
Subsonic speed
Transonic speed
Venting
Vents