메뉴 건너뛰기




Volumn 44, Issue , 2011, Pages 505-526

Multidisciplinary optimization with applications to sonic-boom minimization

Author keywords

Aircraft design; Boom propagation; Noise; Perceived loudness; Robust design; Supersonic design; Supersonic flow

Indexed keywords

AIRCRAFT DESIGN; CURRENT STATUS; HUMAN EAR; KEY CONSTRAINTS; MAN-MADE STRUCTURES; MULTI-DISCIPLINARY OPTIMIZATIONS; NOISE; PERCEIVED LOUDNESS; PRESSURE DISTURBANCE; RESEARCH EFFORTS; ROBUST DESIGNS; SONIC BOOMS;

EID: 84555196963     PISSN: 00664189     EISSN: None     Source Type: Book Series    
DOI: 10.1146/annurev-fluid-120710-101133     Document Type: Article
Times cited : (63)

References (54)
  • 1
    • 85088185199 scopus 로고    scopus 로고
    • Advanced algorithms for design and optimization of quiet supersonic platforms
    • 40th, Reno, NV, AIAA Pap.
    • Alonso J, Kroo I, Jameson A. 2002. Advanced algorithms for design and optimization of quiet supersonic platforms. Presented at AIAA Aerosp. Sci. Meet. Exhib., 40th, Reno, NV, AIAA Pap. 2002-0144
    • (2002) AIAA Aerosp. Sci. Meet. Exhib. , pp. 2002-0144
    • Alonso, J.1    Kroo, I.2    Jameson, A.3
  • 2
    • 22544484509 scopus 로고    scopus 로고
    • Two supersonic business aircraft conceptual designs, with and without sonic boom constraint
    • Aronstein D, Schueler K. 2005. Two supersonic business aircraft conceptual designs, with and without sonic boom constraint. J. Aircr. 42:775-86 (Pubitemid 41013381)
    • (2005) Journal of Aircraft , vol.42 , Issue.3 , pp. 775-786
    • Aronstein, D.C.1    Schueler, K.L.2
  • 4
    • 85067317820 scopus 로고    scopus 로고
    • Efficient unstructured grid adaptation methods for sonic boom prediction
    • 26th, Honolulu, AIAA Pap.
    • Campbell R, Carter M, Deere K, Waithe K. 2008. Efficient unstructured grid adaptation methods for sonic boom prediction. Presented at AIAA Appl. Aerodyn. Conf., 26th, Honolulu, AIAA Pap. 2008-7327
    • (2008) AIAA Appl. Aerodyn. Conf. , pp. 2008-7327
    • Campbell, R.1    Carter, M.2    Deere, K.3    Waithe, K.4
  • 7
    • 54549108980 scopus 로고    scopus 로고
    • Evolutionary-based multidisciplinary design exploration for the silent supersonic technology demonstrator wing
    • Chiba K, Makino Y, Takatoya T. 2008. Evolutionary-based multidisciplinary design exploration for the silent supersonic technology demonstrator wing. J. Aircr. 45:1481-94
    • (2008) J. Aircr. , vol.45 , pp. 1481-1494
    • Chiba, K.1    Makino, Y.2    Takatoya, T.3
  • 8
    • 42949144866 scopus 로고    scopus 로고
    • Multifidelity design optimization of low-boom supersonic jets
    • DOI 10.2514/1.28948
    • Choi S, Alonso J, Kroo I, Wintzer M. 2008. Multifidelity design optimization of low-boom supersonic jets. J. Aircr. 45:106-18 (Pubitemid 351607263)
    • (2008) Journal of Aircraft , vol.45 , Issue.1 , pp. 106-118
    • Choi, S.1    Alonso, J.J.2    Kroo, U.M.3    Wintzer, M.4
  • 9
    • 73349088985 scopus 로고    scopus 로고
    • Numerical and mesh resolution requirements for accurate sonic boom prediction
    • Choi S, Alonso JJ, van der Weide E. 2009. Numerical and mesh resolution requirements for accurate sonic boom prediction. J. Aircr. 46:1126-39
    • (2009) J. Aircr. , vol.46 , pp. 1126-1139
    • Choi, S.1    Alonso, J.J.2    Van Der Weide, E.3
  • 10
    • 16244418354 scopus 로고    scopus 로고
    • Design of low-boom supersonic business jet with evolutionary algorithms using adaptive unstructured mesh
    • 45th, Palm Springs, CA, AIAA Pap.
    • Choi S, Chung HS, Alonso JJ. 2004. Design of low-boom supersonic business jet with evolutionary algorithms using adaptive unstructured mesh. Presented at AIAA/ASME/ASCE/AHS/ASC Struct., Struct. Dyn. Mater. Conf., 45th, Palm Springs, CA, AIAA Pap. 2004-1758
    • (2004) AIAA/ASME/ASCE/AHS/ASC Struct., Struct. Dyn. Mater. Conf. , pp. 2004-1758
    • Choi, S.1    Chung, H.S.2    Alonso, J.J.3
  • 11
    • 85085402699 scopus 로고    scopus 로고
    • Design of a low-boom supersonic business jet using Cokriging approximation models
    • 9th, Atlanta, AIAA Pap
    • Chung HS, Alonso JJ. 2002. Design of a low-boom supersonic business jet using Cokriging approximation models. Presented at AIAA/ISSMO Symp. Multidiscip. Anal. Optim., 9th, Atlanta, AIAA Pap. 2002-5598
    • (2002) AIAA/ISSMO Symp. Multidiscip. Anal. Optim. , pp. 2002-5598
    • Chung, H.S.1    Alonso, J.J.2
  • 13
    • 84880818213 scopus 로고    scopus 로고
    • Sonic boom minimization revisited: The robustness of optimal low-boom designs
    • 13th, Fort Worth, TX, AIAA Pap
    • Colonno M, Alonso J. 2010. Sonic boom minimization revisited: the robustness of optimal low-boom designs. Presented at AIAA/ISSMO Multidiscip. Anal. Optim. Conf., 13th, Fort Worth, TX, AIAA Pap. 2010-9364
    • (2010) AIAA/ISSMO Multidiscip. Anal. Optim. Conf. , pp. 2010-9364
    • Colonno, M.1    Alonso, J.2
  • 14
    • 78149421180 scopus 로고    scopus 로고
    • The challenges of defining an acceptable sonic boom overland
    • 15th, Miami, AIAA Pap.
    • Coulouvrat F, 2009. The challenges of defining an acceptable sonic boom overland. Presented at AIAA/CEAS Aeroacoust. Conf. (30th AIAA Aeroacoust. Conf.), 15th, Miami, AIAA Pap. 2009-3384
    • (2009) AIAA/CEAS Aeroacoust. Conf. (30th AIAA Aeroacoust. Conf.) , pp. 2009-3384
    • Coulouvrat, F.1
  • 15
    • 45849150655 scopus 로고    scopus 로고
    • An overview of the Gulfstream/NASA quiet spike flight test program
    • 46th, Reno, NV, AIAA Pap
    • Cowart R, Grindle T. 2008. An overview of the Gulfstream/NASA quiet spike flight test program. Presented at AIAA Aerosp. Sci. Meet. Exhib., 46th, Reno, NV, AIAA Pap. 2008-123
    • (2008) AIAA Aerosp. Sci. Meet. Exhib. , pp. 2008-2123
    • Cowart, R.1    Grindle, T.2
  • 16
    • 49349086292 scopus 로고
    • Minimization of sonic-boom parameters in real and isothermal atmospheres
    • NASA
    • Darden C, 1975. Minimization of sonic-boom parameters in real and isothermal atmospheres. Tech. Rep. TN D-7842, NASA
    • (1975) Tech. Rep. TN D-7842
    • Darden, C.1
  • 17
    • 0017504481 scopus 로고
    • Sonic boom theory: Its status in prediction and minimization
    • Darden C. 1977. Sonic boom theory: its status in prediction and minimization. J. Aircr. 14:569-76
    • (1977) J. Aircr. , vol.14 , pp. 569-576
    • Darden, C.1
  • 18
  • 19
    • 85006409852 scopus 로고
    • Sonic boom minimization including both front and rear shocks
    • George A, Seebass R. 1971. Sonic boom minimization including both front and rear shocks. AIAA Tech. Notes 9:2091-93
    • (1971) AIAA Tech. Notes , vol.9 , pp. 2091-2093
    • George, A.1    Seebass, R.2
  • 21
    • 36949074468 scopus 로고
    • The 'double bang' of supersonic aircraft
    • Gold T. 1952. The 'double bang' of supersonic aircraft. Nature 170:808
    • (1952) Nature , vol.170 , pp. 808
    • Gold, T.1
  • 22
    • 0008086365 scopus 로고
    • Linearized supersonic flow
    • Calif. Inst. Technol
    • Hayes W, 1947. Linearized supersonic flow. North Am. Aviat. Rep. AL-222, Calif. Inst. Technol.
    • (1947) North Am. Aviat. Rep. AL-222
    • Hayes, W.1
  • 23
  • 24
    • 85087188716 scopus 로고    scopus 로고
    • The case for small supersonic civil aircraft
    • Dayton, OH, AIAA Pap
    • Henne P. 2003. The case for small supersonic civil aircraft. Presented at AIAA/ICAS Int. Air Space Symp. Expo., Dayton, OH, AIAA Pap. 2003-2555
    • (2003) AIAA/ICAS Int. Air Space Symp. Expo. , pp. 2003-2555
    • Henne, P.1
  • 25
    • 22544488412 scopus 로고    scopus 로고
    • Case for small supersonic civil aircraft
    • Henne P, 2005. Case for small supersonic civil aircraft. J. Aircr. 42:765-74 (Pubitemid 41013380)
    • (2005) Journal of Aircraft , vol.42 , Issue.3 , pp. 765-774
    • Henne, P.A.1
  • 26
    • 45849112782 scopus 로고    scopus 로고
    • Quiet spike near field flight test pressure measurements with computational fluid dynamics comparisons
    • 46th, Reno, NV, AIAA Pap
    • Howe D, Waithe K, Haering E. 2008. Quiet spike near field flight test pressure measurements with computational fluid dynamics comparisons. Presented at AIAA Aerosp. Sci. Meet. Exhib., 46th, Reno, NV, AIAA Pap. 2008-128
    • (2008) AIAA Aerosp. Sci. Meet. Exhib. , pp. 2008-2128
    • Howe, D.1    Waithe, K.2    Haering, E.3
  • 27
    • 33751437885 scopus 로고
    • Lower bounds for sonic bangs
    • Jones L, 1961. Lower bounds for sonic bangs. J. R. Aeronaut. Soc. 65:1-4
    • (1961) J. R. Aeronaut. Soc. , vol.65 , pp. 1-4
    • Jones, L.1
  • 28
    • 0345649238 scopus 로고
    • Theory of wing-body drag at supersonic speeds
    • NACA
    • Jones R, 1953. Theory of wing-body drag at supersonic speeds. Tech. Rep. RM A53H18a, NACA
    • (1953) Tech. Rep. RM A53H18a
    • Jones, R.1
  • 29
    • 84871824389 scopus 로고    scopus 로고
    • Feasibility study of using a small-scale UAS for sonic boom minimization research
    • 49th, Orlando, FL, AIAA Pap
    • Jung T, Starkey R, Argrow B. 2011. Feasibility study of using a small-scale UAS for sonic boom minimization research. Presented at AIAA Aerosp. Sci. Meet., 49th, Orlando, FL, AIAA Pap. 2011-1280
    • (2011) AIAA Aerosp. Sci. Meet. , pp. 2011-1280
    • Jung, T.1    Starkey, R.2    Argrow, B.3
  • 30
    • 49349089774 scopus 로고    scopus 로고
    • Interactive inverse design optimization of fuselage shape for low-boom supersonic concepts
    • Li W, Shields E, Le D. 2008. Interactive inverse design optimization of fuselage shape for low-boom supersonic concepts. J. Aircr. 45:1381-97
    • (2008) J. Aircr. , vol.45 , pp. 1381-1397
    • Li, W.1    Shields, E.2    Le, D.3
  • 31
    • 33750840579 scopus 로고    scopus 로고
    • Robust objective functions for sonic-boom minimization
    • DOI 10.2514/1.19442
    • Makino Y, Kroo I. 2006. Robust objective functions for sonic-boom minimization. J. Aircr. 43:1301-6 (Pubitemid 44713936)
    • (2006) Journal of Aircraft , vol.43 , Issue.5 , pp. 1301-1306
    • Makino, Y.1    Kroo, I.2
  • 32
    • 78149440264 scopus 로고
    • Some nonasymptotic effects on the sonic boom of large aircraft
    • NASA
    • McLean FE, 1965. Some nonasymptotic effects on the sonic boom of large aircraft. Tech. Rep. NASA/TN D-2877, NASA
    • (1965) Tech. Rep. NASA/TN D-2877
    • McLean, F.E.1
  • 33
    • 33846200263 scopus 로고
    • Configuration design for specified pressure signature characteristics
    • NASA
    • McLean FE. 1968. Configuration design for specified pressure signature characteristics. Tech. Rep. NASA/SP 180, NASA
    • (1968) Tech. Rep. NASA/SP 180
    • McLean, F.E.1
  • 34
    • 84555162982 scopus 로고    scopus 로고
    • Final report for the advanced concept studies for supersonic commercial transports entering service in the 2030 to 2035 period, N+3 supersonic program
    • Lockheed Martin Aeronaut. Co. Natl. Res. Council 1997. U.S. supersonic commercial aircraft: assessing NASA's high speed research program. Tech. Rep., Natl. Res. Council, Washington DC
    • Morgenstern J, Norstrud N, Stelmack M, Skoch C. 2010. Final report for the advanced concept studies for supersonic commercial transports entering service in the 2030 to 2035 period, N+3 supersonic program. Tech. Rep. NASA/CR 2010-216796, Lockheed Martin Aeronaut. Co. Natl. Res. Council. 1997. U.S. supersonic commercial aircraft: assessing NASA's high speed research program. Tech. Rep., Natl. Res. Council, Washington, DC
    • (2010) Tech. Rep. NASA/CR 2010-216796
    • Morgenstern, J.1    Norstrud, N.2    Stelmack, M.3    Skoch, C.4
  • 35
    • 34250864483 scopus 로고    scopus 로고
    • Sonic boom prediction using Euler/full potential methodology
    • 45th, Reno, NV, AIAA Pap
    • Ozcer I. 2007. Sonic boom prediction using Euler/full potential methodology. Presented at AIAA Aerosp. Sci. Meet. Exhib., 45th, Reno, NV, AIAA Pap. 2007-369
    • (2007) AIAA Aerosp. Sci. Meet. Exhib. , pp. 2007-2369
    • Ozcer, I.1
  • 36
  • 37
    • 33744659658 scopus 로고
    • Review of sonic boom theory
    • 12th, San Antonio, TX, AIAA Pap.
    • Plotkin K, 1989. Review of sonic boom theory. Presented at Aeroacoust. Conf., 12th, San Antonio, TX, AIAA Pap. 89-1105
    • (1989) Aeroacoust. Conf. , pp. 89-1105
    • Plotkin, K.1
  • 38
    • 85088760839 scopus 로고    scopus 로고
    • Extrapolation of sonic boom signatures from CFD solutions
    • 40th, Reno, NV, AIAA Pap
    • Plotkin K, 2002. Extrapolation of sonic boom signatures from CFD solutions. Presented at AIAA Aerosp. Sci. Meet. Exhib., 40th, Reno, NV, AIAA Pap. 2002-922
    • (2002) AIAA Aerosp. Sci. Meet. Exhib. , pp. 2002-2922
    • Plotkin, K.1
  • 39
    • 82555188330 scopus 로고    scopus 로고
    • Advanced sonic boom prediction using augmented Burger's equation
    • Orlando, FL, AIAA Pap.
    • Rallabhandi S, 2011. Advanced sonic boom prediction using augmented Burger's equation. Presented at 49th AIAA Aerosp. Sci. Meet., Orlando, FL, AIAA Pap. 2011-1278
    • (2011) 49th AIAA Aerosp. Sci. Meet. , pp. 2011-1278
    • Rallabhandi, S.1
  • 40
    • 0032713611 scopus 로고    scopus 로고
    • Constrained multipoint aerodynamic shape optimization using an adjoint formulation and parallel computers, parts 1 and 2
    • Reuther JJ, Jameson A, Alonso JJ, Rimlinger MJ, Saunders D. 1999. Constrained multipoint aerodynamic shape optimization using an adjoint formulation and parallel computers, parts 1 and 2. AIAA J. Aircr. 36:51-74
    • (1999) AIAA J. Aircr. , vol.36 , pp. 51-74
    • Reuther, J.J.1    Jameson, A.2    Alonso, J.J.3    Rimlinger, M.J.4    Saunders, D.5
  • 41
    • 84555213159 scopus 로고
    • The design or operation of aircraft to minimize their sonic boom
    • St. Louis, AIAA Pap
    • Seebass A, 1973. The design or operation of aircraft to minimize their sonic boom. Presented at 5th AIAA Aircr. Des., Flight Test, Oper. Meet., St. Louis, AIAA Pap. 1973-817
    • (1973) 5th AIAA Aircr. Des., Flight Test, Oper. Meet. , pp. 1973-1817
    • Seebass, A.1
  • 42
    • 34250889989 scopus 로고    scopus 로고
    • Sonic boom minimization revisited
    • 2nd, Albuquerque, NM, AIAA Pap
    • Seebass A, Argrow B. 1998. Sonic boom minimization revisited. Presented at Theoret. Fluid Mech. Meet., 2nd, Albuquerque, NM, AIAA Pap. 1998-2956
    • (1998) Theoret. Fluid Mech. Meet. , pp. 1998-2956
    • Seebass, A.1    Argrow, B.2
  • 43
    • 84880784152 scopus 로고
    • Sonic boom reduction through aircraft design and operation
    • 11th, Washington, DC, AIAA Pap
    • Seebass A, George A. 1973. Sonic boom reduction through aircraft design and operation. AIAA Aerosp. Sci. Meet., 11th, Washington, DC, AIAA Pap. 1973-241
    • (1973) AIAA Aerosp. Sci. Meet. , pp. 1973-1241
    • Seebass, A.1    George, A.2
  • 44
    • 0016099684 scopus 로고
    • Design and operation of aircraft to minimize their sonic boom
    • Seebass A, George A. 1974. Design and operation of aircraft to minimize their sonic boom. J. Aircr. 11:509-17
    • (1974) J. Aircr. , vol.11 , pp. 509-517
    • Seebass, A.1    George, A.2
  • 45
    • 0014675815 scopus 로고
    • Minimum sonic boom shock strengths and overpressures
    • Seebass R, 1969a. Minimum sonic boom shock strengths and overpressures. Nature 221:651-53
    • (1969) Nature , vol.221 , pp. 651-653
    • Seebass, R.1
  • 46
    • 85003220379 scopus 로고
    • Sonic boom theory
    • Seebass R, 1969b. Sonic boom theory. J. Aircr. 6:177-84
    • (1969) J. Aircr. , vol.6 , pp. 177-184
    • Seebass, R.1
  • 48
    • 84883669715 scopus 로고    scopus 로고
    • Evaluating market and environmental impacts of an N+3 supersonic aircraft
    • 49th, Orlando, FL, AIAA Pap
    • Tetzloff I, Crossley W. 2011. Evaluating market and environmental impacts of an N+3 supersonic aircraft. Presented at AIAA Aerosp. Sci. Meet. Exhib., 49th, Orlando, FL, AIAA Pap. 2011-463
    • (2011) AIAA Aerosp. Sci. Meet. Exhib. , pp. 2011-2463
    • Tetzloff, I.1    Crossley, W.2
  • 49
    • 0003698564 scopus 로고
    • Extrapolation of sonic boom pressure signatures by the waveform parameter method
    • NASA
    • Thomas C, 1972. Extrapolation of sonic boom pressure signatures by the waveform parameter method. Tech. Rep. D-6832, NASA
    • (1972) Tech. Rep. D-6832
    • Thomas, C.1
  • 50
    • 36949074782 scopus 로고
    • Noise from aircraft at supersonic speeds
    • Warren CHE. 1953. Noise from aircraft at supersonic speeds. Nature 171:214-16
    • (1953) Nature , vol.171 , pp. 214-216
    • Warren, C.H.E.1
  • 51
    • 78649516151 scopus 로고    scopus 로고
    • Supersonic vehicle systems for the 2020 to 2035 timeframe
    • 28th, Chicago, AIAA Pap
    • Welge H, Nelson C, Bonet J. 2010. Supersonic vehicle systems for the 2020 to 2035 timeframe. Presented at AIAA Appl. Aerodyn. Conf., 28th, Chicago, AIAA Pap. 2010-4930
    • (2010) AIAA Appl. Aerodyn. Conf. , pp. 2010-4930
    • Welge, H.1    Nelson, C.2    Bonet, J.3
  • 52
    • 84980073009 scopus 로고
    • The flow pattern of a supersonic projectile
    • Whitham G, 1952. The flow pattern of a supersonic projectile. Commun. Pure Appl. Math. 5:301-48
    • (1952) Commun. Pure Appl. Math. , vol.5 , pp. 301-348
    • Whitham, G.1
  • 53
    • 84555213158 scopus 로고    scopus 로고
    • Adjoint-based adaptive mesh refinement for sonic boom prediction
    • 26th, Honolulu, AIAA Pap
    • Wintzer M, Nemec M, Aftosmis M. 2010. Adjoint-based adaptive mesh refinement for sonic boom prediction. Presented at AIAA Appl. Aerodyn. Conf., 26th, Honolulu, AIAA Pap. 2008-6593
    • (2010) AIAA Appl. Aerodyn. Conf. , pp. 2008-6593
    • Wintzer, M.1    Nemec, M.2    Aftosmis, M.3
  • 54
    • 73849150195 scopus 로고    scopus 로고
    • Sonic boom variability due to homogeneous atmospheric turbulence
    • Yamashita H, Obayashi S. 2009. Sonic boom variability due to homogeneous atmospheric turbulence. J. Aircr. 46:1886-93
    • (2009) J. Aircr. , vol.46 , pp. 1886-1893
    • Yamashita, H.1    Obayashi, S.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.