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There are a total of 6 record(s) matching your query.
Sorted by: Date Added To NTRS in Descending order
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Propulsion-induced effects caused by out-of-ground effects
Author(s): Margason, Richard
Abstract: Propulsion induced effects encountered by moderate- to high-disk loading STOVL or VSTOL aircraft out-of-ground effect during hover and transition between hover and wing-borne flight are discussed. Descriptions of the fluid ...
NASA Center: Ames Research Center Publication Year: 1987
Added to NTRS: 2005-10-13
Accession Number: 88N14088; Document ID: 19880004706; Report Number: A-87359, NAS 1.15:100032, NASA-TM-100032
Application of empirical and linear methods to VSTOL powered-lift aerodynamics
Author(s): Margason, Richard; Kuhn, Richard
Abstract: Available prediction methods applied to problems of aero/propulsion interactions for short takeoff and vertical landing (STOVL) aircraft are critically reviewed and an assessment of their strengths and weaknesses provided. ...
NASA Center: Ames Research Center Publication Year: 1988
Added to NTRS: 2005-10-13
Accession Number: 88N17581; Document ID: 19880008197; Report Number: A-88038, NAS 1.15:100048, NASA-TM-100048
Propulsion-induced effects caused by out-of-ground effects
Author(s): Margason, Richard
Abstract: Propulsion induced effects encountered by moderate- to high-disk loading STOVL or VSTOL aircraft out-of-ground effect during hover and transition between hover and wing-borne flight are discussed. Descriptions of the fluid ...
NASA Center: Ames Research Center Publication Year: 1988
Added to NTRS: 2004-11-03
Accession Number: 88A37179; Document ID: 19880049952; Report Number: SAE PAPER 872307
Comparison of Aero/Propulsion Transition Characteristics for a Joint Strike Fighter Configuration
Author(s): Naumowicz, Tim; Margason, Richard; Wardwell, Doug; Hange, Craig; Arledge, Tom
Abstract: NASA Ames conducted a series tests of a large-scale powered model of Lockheed Martin Skunk Works' JSF STOVL configuration at the 80- by 120-Foot Wind Tunnel. The model uses a modified version of an F-16 fighter engine (a ...
NASA Center: Ames Research Center Publication Year: 1996
Added to NTRS: 2004-11-03
Document ID: 20020041011
Comparison of Hover/Ground-Effect Characteristics for a Joint Strike Fighter Configuration
Author(s): Hange, Craig; Naumowicz, Tim; Wardwell, Douglas; Margason, Richard; Arledge, Tom
Abstract: Hover and ground-effect tests were conducted with the Lockheed-Martin Large Scale Powered Model (LSPM) during June-November 1995 at the NASA Ames Research Center's Outdoor Aerodynamics Research Facility (OARF). This was done ...
NASA Center: Ames Research Center Publication Year: 1996
Added to NTRS: 2004-11-03
Document ID: 20020040904
Application of empirical and linear methods to VSTOL powered-lift aerodynamics
Author(s): Margason, Richard; Kuhn, Richard
Abstract: Available prediction methods applied to problems of aero/propulsion interactions for short takeoff and vertical landing (STOVL) aircraft are critically reviewed and an assessment of their strengths and weaknesses provided. ...
NASA Center: Ames Research Center Publication Year: 1988
Added to NTRS: 2004-11-03
Accession Number: 88A37236; Document ID: 19880050009; Report Number: SAE PAPER 872341
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