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Volumn , Issue , 2008, Pages

FUN3D / OptiGRID coupling for unstructured grid adaptation for sonic boom problems

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL PERFORMANCE; CONE-CYLINDER-CONE; DELTA WINGS; FEATURE-BASED; FLOW FEATURES; FLOW SOLVER; GRID ADAPTATION; MID-FIELD; NEAR-FIELD; NORTHROP GRUMMAN; PARALLEL PROCESSING; PRESSURE SIGNAL; SHOCK DETECTIONS; SONIC BOOMS; UNSTRUCTURED FLOW; UNSTRUCTURED GRID; USER INVOLVEMENT;

EID: 78149446233     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (19)

References (22)
  • 2
    • 85087191844 scopus 로고    scopus 로고
    • Prediction of sonic boom signature using euler-full potential CFD with grid adaptation and shock fitting
    • AIAA-2002-2543, Breckenridge, CO: AIAA
    • Kandil, O., A., Yang, Z., Bobbitt, P., J. Prediction of Sonic Boom Signature Using Euler-Full Potential CFD With Grid Adaptation and Shock Fitting. in 8th AIAA/CEAS Aeroacoustics Conference AIAA-2002-2543, 2002. Breckenridge, CO: AIAA.
    • (2002) 8th AIAA/CEAS Aeroacoustics Conference
    • Kandil, O.A.1    Yang, Z.2    Bobbitt, P.J.3
  • 3
    • 34250881745 scopus 로고    scopus 로고
    • and Old Dominion University. Dept. of Aerospace Engineering., Old Dominion University, 2005., 202 leaves
    • Ozcer, I.A. and Old Dominion University. Dept. of Aerospace Engineering., Sonic boom prediction using Euler/full potential methodology. 2005, Old Dominion University, 2005. p. xvi, 202 leaves.
    • (2005) Sonic Boom Prediction Using Euler/full Potential Methodology
    • Ozcer, I.A.1
  • 5
    • 85067317817 scopus 로고    scopus 로고
    • Supersonic business jet design using a knowledge-based genetic algorithm with an adaptive, unstructured grid methodology
    • AIAA-2003-3791, Orlando, Florida: AIAA
    • Chung, H.S., Choi, S., Alonso, J. J. Supersonic Business Jet Design using a Knowledge-Based Genetic Algorithm with an Adaptive, Unstructured Grid Methodology. in 21st Applied Aerodynamics Conference, AIAA-2003-3791, 2003. Orlando, Florida: AIAA.
    • (2003) 21st Applied Aerodynamics Conference
    • Chung, H.S.1    Choi, S.2    Alonso, J.J.3
  • 6
    • 34250876071 scopus 로고    scopus 로고
    • Numerical and mesh resolution requirements for accurate sonic boom prediction of complete aircraft configurations
    • AIAA-2004-1060, Reno, NV: AIAA
    • Choi, S., Alonso, J. J., Weide, E. V. Numerical and Mesh Resolution Requirements for Accurate Sonic Boom Prediction of Complete Aircraft Configurations. in 42nd Aerospace Sciences Meeting and Exhibit, AIAA-2004-1060, 2004. Reno, NV: AIAA.
    • (2004) 42nd Aerospace Sciences Meeting and Exhibit
    • Choi, S.1    Alonso, J.J.2    Weide, E.V.3
  • 7
    • 34250761728 scopus 로고    scopus 로고
    • Efficient anisotropic mesh adaptation on weak and multiple shocks
    • AIAA-2004-0084, Reno, NV: AIAA
    • Remaki, L., Lepage, C., Habashi, W. G. Efficient Anisotropic Mesh Adaptation on Weak and Multiple Shocks. in 42nd Aerospace Sciences Meeting and Exhibit, AIAA-2004-0084, 2004. Reno, NV: AIAA.
    • (2004) 42nd Aerospace Sciences Meeting and Exhibit
    • Remaki, L.1    Lepage, C.2    Habashi, W.G.3
  • 8
    • 28844499993 scopus 로고    scopus 로고
    • Application of parallel adjoint-based error estimation and anisotropic grid adaptation for three-dimensional aerospace configurations
    • AIAA-2005-4842, Toronto, Ontario: AIAA
    • Lee-Rausch, E.M., Park, M. A., Jones, W. T., Hammond, D. P., Nielsen, E. J. Application of Parallel Adjoint-Based Error Estimation and Anisotropic Grid Adaptation for Three-Dimensional Aerospace Configurations. in 23rd AIAA Applied Aerodynamics Conference, AIAA-2005-4842, 2005. Toronto, Ontario: AIAA.
    • (2005) 23rd AIAA Applied Aerodynamics Conference
    • Lee-Rausch, E.M.1    Park, M.A.2    Jones, W.T.3    Hammond, D.P.4    Nielsen, E.J.5
  • 9
    • 34250864424 scopus 로고    scopus 로고
    • Validation of 3D adjoint based error estimation and mesh adaptation for sonic boom prediction
    • AIAA-2006-1150, Reno, NV: AIAA
    • Jones, W.T., Nielsen, E. J., Park, M. A. Validation of 3D adjoint based error estimation and mesh adaptation for sonic boom prediction. in 44th AIAA Aerospace Sciences Meeting and Exhibit, AIAA-2006-1150, 2006. Reno, NV: AIAA.
    • (2006) 44th AIAA Aerospace Sciences Meeting and Exhibit
    • Jones, W.T.1    Nielsen, E.J.2    Park, M.A.3
  • 11
    • 30744475230 scopus 로고    scopus 로고
    • Origins and overview of the shaped sonic boom demonstration program
    • AIAA-2005-0005, Reno, NV
    • Pawlowski, J.W., Graham, D. H. Origins and Overview of the Shaped Sonic Boom Demonstration Program. in 43rd AIAA Aerospace Sciences Meeting, AIAA-2005-0005, 2005. Reno, NV.
    • (2005) 43rd AIAA Aerospace Sciences Meeting
    • Pawlowski, J.W.1    Graham, D.H.2
  • 12
    • 34250856853 scopus 로고    scopus 로고
    • Sonic boom computations for double-cone configuration using CFL3D, FUN3D and full potential codes
    • AIAA-2006-414, Reno, NV: AIAA
    • Kandil, O.A., Ozcer, I. A. Sonic Boom Computations for Double-Cone Configuration using CFL3D, FUN3D and Full Potential Codes. in 44th AIAA Aerospace Sciences Meeting and Exhibit, AIAA-2006-414, 2006. Reno, NV: AIAA.
    • (2006) 44th AIAA Aerospace Sciences Meeting and Exhibit
    • Kandil, O.A.1    Ozcer, I.A.2
  • 13
    • 0020822159 scopus 로고
    • An efficient, full-potential implicit method based on characteristics for supersonic flows
    • Shankar, V., Osher, S., An Efficient, Full-Potential Implicit Method Based on Characteristics for Supersonic Flows. AIAA J 1983. 21(9).
    • (1983) AIAA J , vol.21 , Issue.9
    • Shankar, V.1    Osher, S.2
  • 14
    • 85001752304 scopus 로고
    • An efficient method for incorporating computational fluid dynamics into sonic boom prediction
    • AIAA-91-3275, Baltimore, MD: AIAA
    • Page, J., A., Plotkin, K., J. An Efficient Method for Incorporating Computational Fluid Dynamics Into Sonic Boom Prediction. in AIAA 9th Applied Aerodynamics Conference, AIAA-91-3275, 1991. Baltimore, MD: AIAA.
    • (1991) AIAA 9th Applied Aerodynamics Conference
    • Page, J.A.1    Plotkin, K.J.2
  • 15
    • 84894562634 scopus 로고    scopus 로고
    • The beneficial effects of wing dihedral on sonic boom
    • AIAA 2003-3273, HiltonHead, SC
    • Bobbitt, P., Kandil, O. A. and Yang, Z. The Beneficial Effects of Wing Dihedral on Sonic Boom. in Aeroacoustics Conf., AIAA 2003-3273, 2003. HiltonHead, SC.
    • (2003) Aeroacoustics Conf.
    • Bobbitt, P.1    Kandil, O.A.2    Yang, Z.3
  • 17
    • 34250865664 scopus 로고    scopus 로고
    • Parametric study and effect of nose-piece attachment on sonic boom mitigation
    • AIAA-2007-1243, Reno, NV
    • Ozcer, I.A., Kandil, O. A., Yagiz, B. . Parametric Study and Effect of Nose-Piece Attachment on Sonic Boom Mitigation. in 45th AIAA Aerospace Sciences Meeting and Exhibit, AIAA-2007-1243, 2007. Reno, NV.
    • (2007) 45th AIAA Aerospace Sciences Meeting and Exhibit
    • Ozcer, I.A.1    Kandil, O.A.2    Yagiz, B.3
  • 22
    • 34250864483 scopus 로고    scopus 로고
    • Sonic boom prediction using euler/full potential methodology
    • AIAA-2007-0369, Reno, Nv: AIAA
    • Ozcer, I.A. Sonic Boom Prediction Using Euler/Full Potential Methodology. in 45th AIAA Aerospace Sciences Meeting and Exhibit, AIAA-2007-0369, 2007. Reno, Nv: AIAA.
    • (2007) 45th AIAA Aerospace Sciences Meeting and Exhibit
    • Ozcer, I.A.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.