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Volumn 1, Issue , 2007, Pages 513-530

Sonic boom reduction via remote inverse adjoint approach

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY CONDITIONS; INVERSE PROBLEMS; PRESSURE DISTRIBUTION; REMOTE SENSING; THREE DIMENSIONAL;

EID: 34250823598     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-56     Document Type: Conference Paper
Times cited : (9)

References (12)
  • 1
    • 85086615377 scopus 로고    scopus 로고
    • A shape optimization methodology for reducing the sonic boom initial pressure rise
    • AIAA paper 02-0145, Reno, NV, January
    • B. Argrow C. Farhat, K. Maute and M. Nikbay. A shape optimization methodology for reducing the sonic boom initial pressure rise. AIAA paper 02-0145, AIAA 40th Aerospace Sciences Meeting and Exhibit, Reno, NV, January 2002.
    • (2002) AIAA 40th Aerospace Sciences Meeting and Exhibit
    • Argrow, B.1    Farhat, C.2    Maute, K.3    Nikbay, M.4
  • 3
    • 0003655741 scopus 로고
    • Numerical solutions of the Euler equations by finite volume methods with Runge-Kutta time stepping schemes
    • AIAA Paper 81-1259, January
    • A. Jameson, W. Schmidt, and E. Turkel. Numerical solutions of the Euler equations by finite volume methods with Runge-Kutta time stepping schemes. AIAA Paper 81-1259, January 1981.
    • (1981)
    • Jameson, A.1    Schmidt, W.2    Turkel, E.3
  • 4
    • 0005914380 scopus 로고    scopus 로고
    • Studies of alternative numerical optimization methods applied to the brachistochrone problem
    • A. Jameson and J. C. Vassberg. Studies of alternative numerical optimization methods applied to the brachistochrone problem. OptiCON 99, 1999.
    • (1999) OptiCON , vol.99
    • Jameson, A.1    Vassberg, J.C.2
  • 5
    • 34250896661 scopus 로고    scopus 로고
    • Development of a quiet supersonic aircraft with technology applications to military and civil aircraft
    • AIAA paper 02-0519, Reno, NV, January
    • S. Komadina, A. Drake, and S. Bruner. Development of a quiet supersonic aircraft with technology applications to military and civil aircraft. AIAA paper 02-0519, AIAA 40th Aerospace Sciences Meeting and Exhibit, Reno, NV, January 2002.
    • (2002) AIAA 40th Aerospace Sciences Meeting and Exhibit
    • Komadina, S.1    Drake, A.2    Bruner, S.3
  • 6
    • 85088722268 scopus 로고    scopus 로고
    • A comparison of the continuous and discrete adjoint approach to automatic aerodynamic optimization
    • AIAA paper 2000-0667, Reno, Nevada, January
    • S. Nadarajah and A. Jameson. A comparison of the continuous and discrete adjoint approach to automatic aerodynamic optimization. AIAA paper 2000-0667, 38th Aerospace Sciences Meeting and Exhibit, Reno, Nevada, January 2000.
    • (2000) 38th Aerospace Sciences Meeting and Exhibit
    • Nadarajah, S.1    Jameson, A.2
  • 7
    • 85088757540 scopus 로고    scopus 로고
    • Studies of the continuous and discrete adjoint approaches to viscous automatic aerodynamic shape optimization
    • AIAA paper 2001-2530, Anaheim, CA, June
    • S. Nadarajah and A. Jameson. Studies of the continuous and discrete adjoint approaches to viscous automatic aerodynamic shape optimization. AIAA paper 2001-2530, 15th. Computational Fluid Dynamics Conference, Anaheim, CA, June 2001.
    • (2001) 15th. Computational Fluid Dynamics Conference
    • Nadarajah, S.1    Jameson, A.2
  • 9
    • 34250861159 scopus 로고    scopus 로고
    • S. Nadarajah, A. Jameson, and J. J. Alonso. An adjoint method for the calculation of remote sensitivities in supersonic flow. AIAA Paper 2002-0261, 40th. Aerospace Sciences Meething and Exhibit, Reno, NV, Jan 2002.
    • S. Nadarajah, A. Jameson, and J. J. Alonso. An adjoint method for the calculation of remote sensitivities in supersonic flow. AIAA Paper 2002-0261, 40th. Aerospace Sciences Meething and Exhibit, Reno, NV, Jan 2002.


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.