Search results for: Hunt, L. Roane (Lewis Roane)
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1
Aerothermal analysis of a wing-elevon cove with variable leakage
Authors: Hunt, L. Roane (Lewis Roane)
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1980Physical Description: 41 pages : illustrations ; 27 cm.Holdings: Loading…
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2
Aerothermal environment in chordwise gaps between split elevons at Mach 6.8
Authors: Hunt, L. Roane (Lewis Roane)
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1980Physical Description: 42 pages : illustrations ; 27 cm.Holdings: Loading…
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3
Cyclic tests of P-bulb end-seal designs for a shuttle-type wing-elevon cove membrane seal
Authors: Hunt, L. Roane (Lewis Roane)
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1979Physical Description: 27 pages : illustrations ; 27 cm.Holdings: Loading…
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4
Aerodynamic pressures and heating rates on surfaces between split elevons at Mach 6.6
Authors: Hunt, L. Roane (Lewis Roane)
Published: National Aeronautics and Space Administration, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1988Physical Description: 1 volume.Holdings: Loading…
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5
Nonlinear filter design
Authors: Hunt, L. Roane (Lewis Roane)
Published: National Aeronautics and Space Administration, 1987Physical Description: 1 volume.Holdings: Loading…
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6
Aerodynamic pressure and heating-rate distributions in tile gaps around chine regions with pressure gradients at a Mach number of 6.6
Authors: Hunt, L. Roane (Lewis Roane)
Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [National Technical Information Service, distributor], 1990Physical Description: 1 volume.Holdings: Loading…
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7
Aerothermal environment in chordwise gaps between split elevons at Mach 6.8
Authors: Hunt, L. Roane (Lewis Roane)
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980Physical Description: 1 online resource (57 pages) : illustrations.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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8
Aerothermal analysis of a wing-elevon cove with variable leakage
Authors: Hunt, L. Roane (Lewis Roane)
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980Physical Description: 1 online resource (41 pages) : illustrations.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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9
Aerothermal tests of a 12.5° cone at Mach 6.7 for various Reynolds numbers, angles of attack, and nose shapes
Authors: Nowak, Robert J., Albertson, Cindy W., Hunt, L. Roane (Lewis Roane)
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985Physical Description: 1 online resource (87 pages) : illustrations.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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10
Aerothermal tests of quilted dome models on a flat plate at a Mach number of 6.5
Authors: Glass, Christopher E.Other Authors: “…Hunt, L. Roane (Lewis Roane)…”
Published: National Aeronautics and Space Administration, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1988
Physical Description: 1 volume.Holdings: Loading…
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11
Aerothermal tests of spherical dome protuberances on a flat plate at a Mach number of 6.5
Authors: Glass, Christopher E.Other Authors: “…Hunt, L. Roane (Lewis Roane)…”
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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12
Nonlinear transformat
Authors: Ford, H.Other Authors: “…Hunt, L. Roane (Lewis Roane)…”
Published: National Aeronautics and Space Administration, Ames Research Center, 1983
Physical Description: 1 volume ; 28 cm.Holdings: Loading…
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13
Aerodynamic heating on the corrugated surface of a 10.2.
Authors: Weinstein, IrvingOther Authors:
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1981Physical Description: 43 unnumbered pages : illustrations ; 28 cm.Holdings: Loading…
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14
Computational method to predict thermodynamic, transport, and flow properties for the modified Langley 8-foot high-temperature tunnel
Authors: Venkateswaran, S.Other Authors: “…Hunt, L. Roane (Lewis Roane)…”
Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [For sale by the National Technical Information Service], 1992
Physical Description: 1 volume.Holdings: Loading…
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15
Aerothermal tests of a 12.5⁰ cone at Mach 6.7 for various Reynolds numbers, angles of attack, and nose shapes
Authors: Nowak, Robert J.Other Authors:
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985Physical Description: 1 volume.Holdings: Loading…
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Related Subjects
Aerothermodynamics
Airplanes
Turbulent boundary layer
Aerodynamic heating
Reusable space vehicles
Aerodynamics, Hypersonic
Boundary layer transition
Cones
Control surfaces
Elevons
Flow distribution
Nonlinear theories
Reynolds number
Wind tunnel tests
Wings
Angle of attack (Aerodynamics)
Chords (geometry)
Computer simulation
Design and construction
Filters (Mathematics)
Flight control
Heat
Hypersonic wind tunnels
Laminar boundary layer
Mathematical models
Noses (Aircraft)
Reentry vehicles
Shock layers
Space Shuttle orbiters
Transmission