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Volumn 38, Issue 8, 2000, Pages 1322-1330

Modeling the response from a cascade to an upstream acoustic disturbance

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC WAVE REFLECTION; ACOUSTIC WAVE TRANSMISSION; ALGEBRA; BOUNDARY CONDITIONS; CASCADES (FLUID MECHANICS); COMPUTER SIMULATION; SUPERSONIC AERODYNAMICS; SUPERSONIC AIRCRAFT;

EID: 0034251315     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1131     Document Type: Article
Times cited : (8)

References (16)
  • 3
    • 0029240072 scopus 로고
    • Prediction of supersonic inlet unstart caused by freestream disturbances
    • Mayer, D. W., and Paynter, G. C., "Prediction of Supersonic Inlet Unstart Caused by Freestream Disturbances," AIAA Journal, Vol. 33, No. 2, 1995, pp. 256-275.
    • (1995) AIAA Journal , vol.33 , Issue.2 , pp. 256-275
    • Mayer, D.W.1    Paynter, G.C.2
  • 10
    • 0003888466 scopus 로고
    • Arnold Engineering Development Center, AEDC-TR-89-15, Arnold AFB, TN, Dec.
    • Cooper, G. K., and Sirbaugh, J. R., "The PARC Code: Theory and Usage," Arnold Engineering Development Center, AEDC-TR-89-15, Arnold AFB, TN, Dec. 1989.
    • (1989) The PARC Code: Theory and Usage
    • Cooper, G.K.1    Sirbaugh, J.R.2
  • 11
    • 0000495258 scopus 로고    scopus 로고
    • Response of a two-dimensional cascade to an upstream disturbance
    • Paynter, G. C., "Response of a Two-Dimensional Cascade to an Upstream Disturbance," AIAA Journal, Vol. 35, No. 3, 1997, pp. 434-440.
    • (1997) AIAA Journal , vol.35 , Issue.3 , pp. 434-440
    • Paynter, G.C.1
  • 15
    • 84916830694 scopus 로고
    • U.S. Air Force Wright Aeronautical Labs., AFWAL-TR-3031, Wright Field, OH, April
    • Hankey, W. L., "Introduction to Computational Aerodynamics," U.S. Air Force Wright Aeronautical Labs., AFWAL-TR-3031, Wright Field, OH, April 1983.
    • (1983) Introduction to Computational Aerodynamics
    • Hankey, W.L.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.