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Volumn , Issue , 2000, Pages

Application of pressure sensitive paint to ice accreted wind tunnel models

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; AIRFOILS; CALIBRATION; FREEZING; ICE; LUMINOUS PAINT; METAL TESTING; NASA; PAINT; SUPERSONIC AERODYNAMICS; TESTING;

EID: 85088760437     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-834     Document Type: Conference Paper
Times cited : (5)

References (8)
  • 5
    • 0031120380 scopus 로고    scopus 로고
    • Temperature and Pressure-Sensitive Luminescent Paints in Aerodynamics
    • Liu, T., Campbell, B.T., Burns, S.P., and Sullivan, J.P., "Temperature and Pressure-Sensitive Luminescent Paints in Aerodynamics, " Applied Mechanics Reviews, 50(4), 227-246, 1997.
    • (1997) Applied Mechanics Reviews , vol.50 , Issue.4 , pp. 227-246
    • Liu, T.1    Campbell, B.T.2    Burns, S.P.3    Sullivan, J.P.4
  • 6
    • 0030290482 scopus 로고    scopus 로고
    • Image Registration for Pressure-Sensitive Paint Applications
    • Bell, J.H., McLachlan, B.G., "Image Registration for Pressure-Sensitive Paint Applications", Exp. in Fluids, 22,78-86.
    • Exp. in Fluids , vol.22 , pp. 78-86
    • Bell, J.H.1    McLachlan, B.G.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.