This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
Implementation of Parametric Anaylsis to the Aerodynamic Design of a Hypersonic Strike Fighter
Technical Paper
2000-01-5561
ISSN: 0148-7191, e-ISSN: 2688-3627
Annotation ability available
Sector:
Language:
English
Abstract
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.
Recommended Content
Authors
Citation
Mavris, D. and Graham, M., "Implementation of Parametric Anaylsis to the Aerodynamic Design of a Hypersonic Strike Fighter," SAE Technical Paper 2000-01-5561, 2000, https://doi.org/10.4271/2000-01-5561.Also In
References
- RFP: Hypersonic Strike Fighter AIAA Foundation Graduate Aircraft Design Competition September 1999
- Pete Hollingsworth, Dimitri Mavris, A Method for Concept Exploration of Hypersonic Vehicles in the Presence of Open & Evolving Requirements 5 th World Aviation Congress and Exposition San Diego, CA October 10-12 2000 2000-01-5560.
- Peter De Baets, Dimitri Mavris, Methodology for the Parametric Conceptual Design of Hypersonic Vehicles 5 th World Aviation Congress and Exposition San Diego, CA October 10-12 2000 2000-01-5618.
- Buckley, M.J. Fertig, K. W. Smith, D. E. Design Sheet: An Environment for Facilitating the Flexible Trade Studies During Conceptual Design AIAA 1992 Aerospace Design Conference Irvine, Ca. February 3 - 6
- Mastin, C. W. Smith, R. E. Sadrehaghighi, I. Wiese, M. R. Geometric Model for a Parametric Study of the Blended-Wing-Body Airplane 14th AIAA Applied Aerodynamics Conference New Orleans, Louisiana June 17-20 1996
- Baker, William B. Jr. Use of Semiempirical Aerodynamic Methods for Preliminary Design AGARD Report
- Cruz, Christopher I. Wilhite, Alan W. Prediction of High-Speed Aerodynamic Characteristics Using the Aerodynamic Preliminary Analysis System (APAS) AIAA 7 th Applied Aerodynamics Conference Seattle, WA July 31 - August 2 1989
- Miranda, Luis R. Elliot, Robert D. Baker, William M. A Generalized Vortex Lattice Method for Subsonic and Supersonic Flow Application NASA Contractor Report 2865 December 1977
- McDonald, Robert Dimitri Mavris, Formulation, Realization, and Demonstration of a Process to Generate Aerodynamic Mete-Models for Hypersonic Cruise Vehicle Design 5 th World Aviation Congress and Exposition San Diego, CA October 10-12 2000 2000-01-5559.