Using response surface metamodels to optimize the aerodynamic performance of a high speed standoff missile within a multi-disciplinary environment

AIAA's Aircraft Technology, Integration, and Operations (ATIO) 2002 Technical Forum

Volumn , Issue , 2002, Pages

  Won, Henry ^a   Levine, Simon ^a   Pfaender, Holger ^b   Mavris, Dimitri N ^b  

^a GEORGIA INSTITUTE OF TECHNOLOGY   (United States)

^b Institute of Aeronautics and Astronautics   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 84894566514     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

1. Roth, B., Mavris, D., "Evaluation and Selection of Technology Concepts for a Hypersonic High Speed Standoff Missile." Presented at 2000 Missile Sciences Conference, Monterey, Ca, 2000.
2. Mavris, D.N., De Laurentis, D.A., Methodology for Examining the Simultaneous Impact of Requirements, Vehicle Characteristics, and Technologies on Military Aircraft Design, Presented at the 22nd Congress of the International Council on the Aeronautical Sciences (ICAS), Harrogate, England, August 27-31, 2000.
3. Ender, T., McClure, E., "Development of an Integrated Parametric Environment for Conceptual High Speed Missile Sizing ", AIAA-2002-5856.
4. M. Moore, J. Williams, Aerodynamic Prediction Rationale for Analyses of Hypersonic Configurations, 27th Aerospace Sciences Meeting, January 9-12, 1989/Reno, Nevada.
5. Middleton, W.D., Lundry, J.L.m Coleman, R.G., "A Computational System for Aerodynamic Design and Analysis of Supersonic Aircraft, Part 2: User's Manual," NASA, 1976.
6. www.engineous.com
7. Fleeman, E. L. "Tactical Missile Design" American Institute of Aeronautics and Astronautics, Reston, VA 2001
8. Michael Montero,"Introduction to Design of Experiments",, summer 2001.