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Implementation of Parametric Anaylsis to the Aerodynamic Design of a Hypersonic Strike Fighter Aerospace Systems Design Laboratory, Georgia Institute of Technology

SAE Technical Papers (1906-current) Available online

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Format:
Book
Conference/Event
Author/Creator:
Mavris, Dimitri, author.
Conference Name:
World Aviation Congress & Exposition (2000-10-10 : San Diego, California, United States)
Language:
English
Physical Description:
1 online resource cm
Place of Publication:
Warrendale, PA SAE International 2000
Summary:
A Hypersonic Strike Fighter (HSF) would provide many benefits over current fighters, including increased effectiveness and survivability. However, there are many design challenges to developing such a vehicle. Therefore the conceptual design of an HSF requires the development of new tools and methods to analyze and select vehicle concepts. A parametric method was developed to determine aerodynamic characteristics of hypersonic vehicles in a rapid, automated way. This parametric method and other tools were then used to select a baseline design and optimize this baseline for the notional mission
Notes:
Vendor supplied data
Publisher Number:
2000-01-5561
Access Restriction:
Restricted for use by site license

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