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Volumn 4, Issue 1, 1997, Pages 51-57

Electrical discharge technique for three-dimensional flow field visualization in hypersonic shock tunnel

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EID: 0001800510     PISSN: 10653090     EISSN: None     Source Type: Journal    
DOI: 10.1615/JFlowVisImageProc.v4.i1.50     Document Type: Article
Times cited : (15)

References (3)
  • 1
    • 0025534855 scopus 로고
    • New Method for Visualizing Three-dimensional Shock Shapes Around Hypersonic Vehicles Using an Electrical Discharge
    • M. Nishio, New Method for Visualizing Three-dimensional Shock Shapes Around Hypersonic Vehicles Using an Electrical Discharge, AIAA J., vol. 28, pp. 2085-2091, 1990.
    • (1990) AIAA J. , vol.28 , pp. 2085-2091
    • Nishio, M.1
  • 2
    • 0024139943 scopus 로고
    • Experimental Real-gas Hypersonics
    • Dec.
    • N. G. Hornung, Experimental Real-gas Hypersonics, Aer. J., pp. 379-389, Dec. 1988.
    • (1988) Aer. J. , pp. 379-389
    • Hornung, N.G.1
  • 3
    • 0000658098 scopus 로고    scopus 로고
    • A New Technique for Visualization of Shock Shapes in Hypersonic Shock Tunnel
    • G. Jagadeesh, B. R. Srinivasa Rao, K. Nagashetty, N. M. Reddy, and K. P. J. Reddy, A New Technique for Visualization of Shock Shapes in Hypersonic Shock Tunnel, Curr. Sci., vol. 71, pp. 128-130, 1996.
    • (1996) Curr. Sci. , vol.71 , pp. 128-130
    • Jagadeesh, G.1    Srinivasa Rao, B.R.2    Nagashetty, K.3    Reddy, N.M.4    Reddy, K.P.J.5


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.