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Volumn 37, Issue 1, 1999, Pages 141-143

Comment on the aeroacoustic formulation of hardin and pope

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EID: 85008270597     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.682     Document Type: Note
Times cited : (81)

References (5)
  • 1
    • 34249772505 scopus 로고
    • An Acoustic/Viscous Splitting Technique for Computational Aeroacoustics
    • Hardin, J. C., and Pope, D. S., "An Acoustic/Viscous Splitting Technique for Computational Aeroacoustics," Theoretical ComputationalFluid Dynamics, Vol. 6, No. 5-6, 1994, pp. 323-340.
    • (1994) Theoretical Computationalfluid Dynamics , vol.6 , Issue.5-6 , pp. 323-340
    • Hardin, J.C.1    Pope, D.S.2
  • 2
    • 0029257040 scopus 로고
    • Sound Generation by Flow over a Two-Dimensional Cavity
    • Hardin, J. C., and Pope, D. S., "Sound Generation by Flow over a Two-Dimensional Cavity," AIAA Journal, Vol. 33, No. 3, 1995, pp. 407-412.
    • (1995) AIAA Journal , vol.33 , Issue.3 , pp. 407-412
    • Hardin, J.C.1    Pope, D.S.2
  • 4
    • 0009132044 scopus 로고    scopus 로고
    • Ph.D. Thesis, Risø-R-947 (EN), Risø National Lab., Roskilde, Denmark, Dec
    • Dahl, K. S., "Aeroacoustic Computation of Low Mach Number Flow," Ph.D. Thesis, Risø-R-947 (EN), Risø National Lab., Roskilde, Denmark, Dec. 1996.
    • (1996) Aeroacoustic Computation of Low Mach Number Flow
    • Dahl, K.S.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.