메뉴 건너뛰기




Volumn 33, Issue 1, 1996, Pages 109-116

Pressure sensitive paint in transonic wind-tunnel testing of the F-15

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; DATABASE SYSTEMS; FLOW VISUALIZATION; PAINT; PRESSURE MEASUREMENT; SURFACES; TRANSONIC FLOW; WIND TUNNELS;

EID: 0029724080     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/3.46910     Document Type: Article
Times cited : (10)

References (8)
  • 2
    • 0005669406 scopus 로고
    • Optical Surface Pressure Measurements: Initial Experience in the MCAIR PSWT
    • The Royal Aeronautical Society, Southampton Univ., UK, Sept. (Paper 12)
    • Crites, R. C., Benne, M. E., Morris, M. J., and Donovan, J. F., "Optical Surface Pressure Measurements: Initial Experience in the MCAIR PSWT," Wind Tunnels and Wind Tunnel Test Techniques, The Royal Aeronautical Society, Southampton Univ., UK, Sept. 1992 (Paper 12).
    • (1992) Wind Tunnels and Wind Tunnel Test Techniques
    • Crites, R.C.1    Benne, M.E.2    Morris, M.J.3    Donovan, J.F.4
  • 8
    • 0027694891 scopus 로고
    • Uncertainty Estimates for Pressure Sensitive Paint Measurements
    • Sabjen, M., "Uncertainty Estimates for Pressure Sensitive Paint Measurements," AIAA Journal, Vol. 31, No. 11, 1993, pp. 2105-2110.
    • (1993) AIAA Journal , vol.31 , Issue.11 , pp. 2105-2110
    • Sabjen, M.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.