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Volumn , Issue , 2001, Pages

Detection of shock motion using laser schlieren system in a hypersonic swbli flowfield

Author keywords

[No Author keywords available]

Indexed keywords

MOTION ANALYSIS; SCHLIEREN SYSTEMS; SHOCK WAVES; SURFACE ANALYSIS;

EID: 85088723672     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-1756     Document Type: Conference Paper
Times cited : (4)

References (11)
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    • Merzkirch, W.1
  • 2
    • 0000572036 scopus 로고
    • Laser schlieren cross-beam measurements in a supersonic jet shear layer
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    • (1970) AIAA Journal , vol.8 , Issue.2 , pp. 2074-2075
    • Funk, B.H.1    Johnston, K.D.2
  • 3
    • 0029180575 scopus 로고
    • Wide angle light scattering in shock-laser interaction
    • J. Panda. Wide angle light scattering in shock-laser interaction. AIAA Journal, Vol.33(No.l2):PP. 2429-2431, 1995.
    • (1995) AIAA Journal , vol.33 , Issue.12 , pp. 2429-2431
    • Panda, J.1
  • 4
    • 0029195039 scopus 로고
    • Shock detection technique based on light Scattering by shock
    • J. Panda. Shock detection technique based on light Scattering by shock. AIAA Journal, Vol.33(No.l2):pp. 2431-2433, 1995.
    • (1995) AIAA Journal , vol.33 , Issue.12 , pp. 2431-2433
    • Panda, J.1
  • 5
    • 85003361443 scopus 로고
    • Real-time op tical measurement of time-dependent shock position
    • M. Sajben and R.C. Crites. Real-time optical measurement of time-dependent shock position. AIAA Journal, 17(8):910-912, 1979.
    • (1979) AIAA Journal , vol.17 , Issue.8 , pp. 910-912
    • Sajben, M.1    Crites, R.C.2
  • 6
    • 0020167940 scopus 로고
    • Comparison of hot-film probe and optical techniques for sensing shock motion
    • F.W. Roos and T.J. Bogar. Comparison of hot-film probe and optical techniques for sensing shock motion. AIAA Journal, 20(8):1071-1076, 1982.
    • (1982) AIAA Journal , vol.20 , Issue.8 , pp. 1071-1076
    • Roos, F.W.1    Bogar, T.J.2
  • 7
    • 0000490638 scopus 로고
    • Fluctuating wall pressure under a separated supersonic flow
    • A.L. Kistler. Fluctuating wall pressure under a separated supersonic flow. Journal of the Acoustical Society of America, 36(No.3):pp. 543-550, 1964.
    • (1964) Journal of the Acous Tical Society of America , vol.36 , Issue.3 , pp. 543-550
    • Kistler, A.L.1
  • 8
    • 0020944128 scopus 로고
    • Unsteadiness of the separation shock wave structure in a super sonic compression ramp field
    • D.S. Dolling and M.T. Murphy. Unsteadiness of the separation shock wave structure in a super sonic compression ramp field. AIAA Journal, Vol. 21(No. 12):pp. 1628-1634, 1983.
    • (1983) AIAA Journal , vol.21 , Issue.12 , pp. 1628-1634
    • Dolling, D.S.1    Murphy, M.T.2
  • 9
    • 84897867323 scopus 로고    scopus 로고
    • Study of flow unsteadiness in a hypersonic swbli flowfield on a hac model
    • AIAA Paper No-2001-0566, Session APA-9, January, Neveda, USA
    • S.B. Verma and G. Koppenwallner. Study of flow unsteadiness in a hypersonic swbli flowfield on a hac model. 39th AIAA Aerospace Sciences Meeting and Exhibit, AIAA Paper No-2001-0566, Session APA-9, January 2001, Neveda, USA.
    • (2001) 39th AIAA Aerospace Sciences Meeting and Exhibit
    • Verma, S.B.1    Koppenwallner, G.2
  • 10
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    • Nature of shock-wave/boundary-layer interaction on a 24° ramp model
    • 15-17 November, University of Stuttgart, Germany
    • S.B. Verma and G. Koppenwallner. Nature of shock-wave/boundary-layer interaction on a 24° ramp model. 12th DGLR-Fach-Symposium der AG-STAB, 15-17 November, University of Stuttgart, Germany.
    • 12th DGLR-Fach-Symposium Der AG-STAB
    • Verma, S.B.1    Koppenwallner, G.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.