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There are a total of 5 record(s) matching your query.
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Aerodynamic Characteristics of a Proposed Personnel Launch System (PLS) Lifting-Body Configuration at Mach Numbers from 0.05 to 20.3. Supplement
Author(s): Cruz, Christopher I.; Ware, George M.; Grafton, Sue B.; Woods, William C.; Young, James C.
Abstract: A wind-tunnel investigation was performed to determine the aerodynamic characteristics of a proposed lifting-body personnel launch system (PLS) configuration over a Mach range of 0.05 to 20.3. The test configuration had a ...
NASA Center: Langley Research Center
Publication Year: 1989
Added to NTRS: 2009-02-25
Document ID: 20090005242; Report Number: NASA-TM-101651
Aerodynamic Characteristics of a Proposed Personnel Launch System (PLS) Lifting-Body Configuration at Mach Numbers from 0.05 to 20.3
Author(s): Cruz, Christopher I.; Ware, George M.; Grafton, Sue B.; Woods, William C.; Young, James C.
Abstract: A wind-tunnel investigation was performed to determine the aerodynamic characteristics of a proposed lifting-body personnel launch system (PLS) configuration over a Mach range of 0.05 to 20.3. The test configuration had a ...
NASA Center: Langley Research Center
Publication Year: 1989
Added to NTRS: 2009-02-10
Accession Number: 93N24522; Document ID: 19930015333; Report Number: NAS 1.15:101641, NASA-TM-101641
Multiaxis thrust vectoring using axisymmetric nozzles and postexit vanes on an F/A-18 configuration vehicle
Author(s): Bowers, Albion H.; Noffz, Gregory K.; Grafton, Sue B.; Mason, Mary L.; Peron, Lee R.
Abstract: A ground-based investigation was conducted on an operational system of multiaxis thrust vectoring using postexit vanes around an axisymmetric nozzle. This thrust vectoring system will be tested on the NASA F/A-18 High Alpha ...
NASA Center: Dryden Flight Research Center, Langley Research Center
Publication Year: 1991
Added to NTRS: 2005-08-25
Accession Number: 91N22083; Document ID: 19910012770; Report Number: H-1705, NAS 1.15:101741, NASA-TM-101741
The F/A-18 High-Angle-of-Attack Ground-to-Flight Correlation; Lessons Learned
Author(s): Banks, Daniel W.; Fisher, David F.; Hall, Robert M.; Erickson, Gary E.; Murri, Daniel G.; Grafton, Sue B.; Sewall, William G.
Abstract: Detailed wind tunnel and flight investigations were performed on the F/A-18 configuration to explore the causes of many high-angle-of-attack phenomena and resulting disparities between wind tunnel and flight results at these ...
NASA Center: Dryden Flight Research Center, Langley Research Center
Publication Year: 1997
Added to NTRS: 2005-08-25
Accession Number: 97N15185; Document ID: 19970009817; Report Number: H-2149, NAS 1.15:4783, NASA-TM-4783
High-alpha flight dynamics research on the X-29 configuration using dynamic model test techniques
Author(s): Croom, Mark A.; Whipple, Raymond D.; Murri, Daniel G.; Grafton, Sue B.; Fratello, David J.
Abstract: High-angle-of-attack flight dynamics of the X-29 configuration were studied using dynamic model test techniques. These tests identified phenomena including wing rock, spins, and tumbling which dominate the high-alpha ...
NASA Center: Langley Research Center
Publication Year: 1988
Added to NTRS: 2004-11-03
Accession Number: 89A51359; Document ID: 19890063988; Report Number: SAE PAPER 881420
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