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There are a total of 13 record(s) matching your query.
Sorted by: Date Added To NTRS in Descending order
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Aerodynamic characteristics of several hypersonic boost-glide-type configurations at Mach numbers from 2.30 to 4.63
Author(s): Carmel, M. M.; Graves, E. B.
Abstract: Aerodynamic characteristics of several hypersonic boostglide configurations at Mach 2.30 to 4.63
NASA Center: Langley Research Center
Publication Year: 1968
Added to NTRS: 2008-05-29
Accession Number: 68N33836; Document ID: 19680024364; Report Number: NASA-TM-X-1601
An investigation of airflow over the aft portions of a variable sweep fighter configuration
Author(s): Graves, E. B.
Abstract: An investigation of air flow over the aft portions of a variable sweep fighter aircraft configuration was made. Tests conducted in the unitary plan wind tunnel at Mach number 2.16 included measurements of forces, moments, ...
NASA Center: NASA (non Center Specific)
Publication Year: 1975
Added to NTRS: 2007-06-25
Accession Number: 76N17022; Document ID: 19760009934; Report Number: NASA-CR-146361
Effect of hypersonic research engine installation on aerodynamic characteristics of 0.0667-scale model of X-15A-2 airplane at Mach numbers from 1.75 to 4.63
Author(s): Graves, E. B.
Abstract: Wind tunnel stability tests to determine effect of hypersonic research engine on aerodynamic characteristics of research aircraft
NASA Center: Langley Research Center
Publication Year: 1969
Added to NTRS: 2007-03-30
Accession Number: 69N38612; Document ID: 19690029227; Report Number: NASA-TM-X-1840
Stability and control characteristics at Mach numbers from 0.20 to 4.63 of a cruciform air-to-air missile with triangular canard controls and a trapezoidal wing
Author(s): Graves, E. B.; Fournier, R. H.
Abstract: Investigations have been conducted in the Langley 8-foot transonic pressure tunnel and the Langley Unitary Plan wind tunnel at Mach numbers from 0.20 to 4.63 to determine the stability and control characteristics of a ...
NASA Center: Langley Research Center
Publication Year: 1974
Added to NTRS: 2005-10-19
Accession Number: 74N33432; Document ID: 19740025319; Report Number: L-9577, NASA-TM-X-3070
Aerodynamic characteristics of a monoplanar missile concept with bodies of circular and elliptical cross sections
Author(s): Graves, E. B.
Abstract: Experimental aerodynamic characteristics of a low-drag missile concept with a body of circular cross section were compared to one with a body of 3:1 elliptical cross section, the bodies having identical cross section area ...
NASA Center: Langley Research Center
Publication Year: 1977
Added to NTRS: 2005-08-25
Accession Number: 78N14999; Document ID: 19780007056; Report Number: L-11423, NASA-TM-74079
Effect of nose bluntness and afterbody shape on aerodynamic characteristics of a monoplanar missile concept with bodies of circular and elliptical cross sections at a Mach number of 2.50
Author(s): Graves, E. B.; Fournier, R. H.
Abstract: The tests were performed at a Mach number of 2.50 and at angles of attack from about -4 deg to 32 deg. The results indicate that increasing nose bluntness increases zero lift drag and decreases both the maximum lift-drag ...
NASA Center: Langley Research Center
Publication Year: 1979
Added to NTRS: 2005-08-25
Accession Number: 79N26023; Document ID: 19790017852; Report Number: L-12632, NASA-TM-80055
Aerodynamic characteristics of a 60 degree swept delta-wing space shuttle orbiter at Mach numbers of 2.50, 3.90, and 4.60
Author(s): Graves, E. B.
Abstract: Wind tunnel tests were performed to determine the static aerodynamic characteristics of a model of a 60 degree swept delta wing space shuttle orbiter. Some control effectiveness tests were included. The tests were conducted ...
NASA Center: Langley Research Center
Publication Year: 1972
Added to NTRS: 2004-11-03
Accession Number: 72N25997; Document ID: 19720018347; Report Number: L-8243, NASA-TM-X-2561
Supersonic aerodynamic characteristics of a two-staged space-shuttle model having a delta-wing orbiter mated atop a winged booster
Author(s): Graves, E. B.
Abstract: An investigation has been conducted in the Langley Unitary Plan wind tunnel to determine the static aerodynamic characteristics of a two-staged space-shuttle system consisting of a delta-wing orbiter mated atop a winged ...
NASA Center: Langley Research Center
Publication Year: 1972
Added to NTRS: 2004-11-03
Accession Number: 72N29995; Document ID: 19720022345; Report Number: L-8300, NASA-TM-X-2569
Supersonic aerodynamic characteristics of a low-aspect-ratio missile model with wing and tail controls and with tails in line and interdigitated
Author(s): Graves, E. B.
Abstract: A study has been made to determine the aerodynamic characteristics of a low-aspect ratio cruciform missile model with all-movable wings and tails. The configuration was tested at Mach numbers from 1.50 to 4.63 with the wings ...
NASA Center: Langley Research Center
Publication Year: 1972
Added to NTRS: 2004-11-03
Accession Number: 72N20971; Document ID: 19720013321; Report Number: L-8092, NASA-TM-X-2531
The feasibility of a high-altitude aircraft platform with consideration of technological and societal constraints
Author(s): Graves, E. B.
Abstract: The feasibility of remotely piloted aircraft performing year around missions at an altitude of 70,000 feet is determined. Blimp and airplane type vehicles employing solar-voltaic, microwave, or nuclear propulsion systems ...
NASA Center: Langley Research Center
Publication Year: 1982
Added to NTRS: 2004-11-03
Accession Number: 82N29313; Document ID: 19820021437; Report Number: NAS 1.15:84508, NASA-TM-84508
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