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Volumn 34, Issue 10, 1996, Pages 2099-2101

Interaction of swept and unswept normal shock waves with boundary layers

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; FINS; FLOW PATTERNS; SHOCK WAVES;

EID: 0030476223     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.13357     Document Type: Article
Times cited : (7)

References (17)
  • 3
    • 0026923557 scopus 로고
    • Physical Model of the Swept Shock Wave Boundary-Layer Interaction Flowfield
    • Alvi, A., and Settles, G. S., "Physical Model of the Swept Shock Wave Boundary-Layer Interaction Flowfield," AIAA Journal, Vol. 30, No. 9, 1992, pp. 2252-2258.
    • (1992) AIAA Journal , vol.30 , Issue.9 , pp. 2252-2258
    • Alvi, A.1    Settles, G.S.2
  • 4
    • 0026627107 scopus 로고
    • A Study of the Interaction of a Normal Shock Wave with a Turbulent Boundary Layer at Mach Numbers between 1.30 and 1.55
    • Atkin, C. J., and Squire, L. C., "A Study of the Interaction of a Normal Shock Wave with a Turbulent Boundary Layer at Mach Numbers Between 1.30 and 1.55," European Journal of Mechanics, B/Fluids, Vol. 11, 1992, pp. 92-118.
    • (1992) European Journal of Mechanics, B/Fluids , vol.11 , pp. 92-118
    • Atkin, C.J.1    Squire, L.C.2
  • 5
    • 0346770798 scopus 로고
    • An Experimental Investigation of the Interaction of an Unsteady Shock with a Turbulent Boundary Layer at Mach Numbers of 1.3 and 1.5
    • Dec.
    • Edwards, J. A., and Squire, L. C., "An Experimental Investigation of the Interaction of an Unsteady Shock with a Turbulent Boundary Layer at Mach Numbers of 1.3 and 1.5," Aeronautical Journal, Vol. 97, Dec. 1993, pp. 337-348.
    • (1993) Aeronautical Journal , vol.97 , pp. 337-348
    • Edwards, J.A.1    Squire, L.C.2
  • 6
    • 0012274446 scopus 로고
    • Possible Types of Flow at Swept Leading Edges
    • Feb.
    • Stanbrook, A., and Squire, L. C., "Possible Types of Flow at Swept Leading Edges," Aeronautical Quarterly, Vol. 15, Feb. 1964, pp. 72-82.
    • (1964) Aeronautical Quarterly , vol.15 , pp. 72-82
    • Stanbrook, A.1    Squire, L.C.2
  • 12
    • 2842550921 scopus 로고
    • Swept Shock/Boundary-Layer Interactions - Scaling Laws, Flowfield Structure and Experimental Methods
    • AGARD Rept. 792
    • Settles, G. S., "Swept Shock/Boundary-Layer Interactions - Scaling Laws, Flowfield Structure and Experimental Methods," Shock-Wave/Boundary-Layer Interactions in Supersonic and Hypersonic Flows, AGARD Rept. 792, 1993.
    • (1993) Shock-Wave/Boundary-Layer Interactions in Supersonic and Hypersonic Flows
    • Settles, G.S.1
  • 15
    • 0005231396 scopus 로고
    • On the Confluence of Three Shock Waves in a Perfect Gas
    • May
    • Henderson, R., "On the Confluence of Three Shock Waves in a Perfect Gas," Aeronautical Quarterly, Vol. 15, May 1964, pp. 181-197.
    • (1964) Aeronautical Quarterly , vol.15 , pp. 181-197
    • Henderson, R.1
  • 16
    • 0038904577 scopus 로고
    • The Three-Shock Confluent on a Simple Wedge Intake
    • Feb.
    • Henderson, R., "The Three-Shock Confluent on a Simple Wedge Intake," Aeronautical Quarterly, Vol. 16, Feb. 1965, pp. 42-54.
    • (1965) Aeronautical Quarterly , vol.16 , pp. 42-54
    • Henderson, R.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.