Sonic boom reduction using an adjoint method for wing-body configurations in supersonic flow

9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization

Volumn , Issue , 2002, Pages

  Nadarajah, Siva K ^a   Jameson, Antony ^a   Alonso, Juan J ^a  

^a 496 Lomita Mall   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY CONDITIONS; INVERSE PROBLEMS; SUPERSONIC AERODYNAMICS; SUPERSONIC AIRCRAFT; SUPERSONIC FLOW;

ADJOINT EQUATIONS; ADJOINT METHODS; GEOMETRY MODIFICATIONS; INVERSE DESIGNS; SONIC-BOOM REDUCTION; SPECIAL TREATMENTS; SUPERSONIC BUSINESS JETS; WING-BODY CONFIGURATIONS;

WINGS;

EID: 85086612989     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-5547     Document Type: Conference Paper

References (8)

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2. F. Marconi, R. Bowersox, M. Orr, J. Mozingo, and J. Schetz Sonic Boom Alleviation using Keel Configurations AIAA 2002-0149, 40th Aerospace Sciences Meeting and Exibit, Reno, Nevada, January 2002.
3. S. Komadina, A. Drake, and S. Bruner Development of a Quiet Supersonic Aircraft with Technology Applications to Military and Civil Aircraft. AIAA 2002-0519, 40th erospace Sciences Meeting and Exibit, Reno, Nevada, January 2002.
4. C. Farhat, K. Maute, B. Argrow, and M. Nikbay A Shape Optimization Methodology for Reducing the Sonic Boom Initial Pressure Rise. AIAA 2002-0145, 40th Aerospace Sciences Meeting and Exibit, Reno, Nevada, January 2002.
5. S. Nadarajah and A. Jameson. A Comparison of the Continuous and Discrete Adjoint Approach to Automatic Aerodynamic Optimization. AIAA 00-0667, AIAA 38th. Aerospace Sciences Meeting and Exhibit, Reno, NV, January 2000.
6. S. Nadarajah and A. Jameson. Studies of the Continuous and Discrete Adjoint Approaches to Viscous Automatic Aerodynamic Shape Optimization AIAA 2001-2530, AIAA 15th. Computational Fluid Dynamic Conference, Anaheim, Ca, June 11-14, 2001.
7. S. Nadarajah, A. Jameson, J. Alonso. An Adjoint Method for the Calculation of Non-Collocated Sensitivities in Supersonic Flow. In Proceedings of First MIT Conference on Computational Fluid and Solid Mechanics, June 12-15, 2001.
8. S. Nadarajah, A. Jameson, and J. Alonso An Adjoint Method for the Calculation of Remote Sensitivities in Supersonic Flow. AIAA 2002-0261, AIAA 40th. Aerospace Sciences Meeting and Exhibit, Reno, NV, January 2002.