메뉴 건너뛰기




Volumn , Issue , 2003, Pages 70-76

Optimization of temperature-sensitive paint formulation for large-scale cryogenic wind tunnels

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER FLOW; COMPUTER SIMULATION; CRACK INITIATION; CRYOGENICS; DYES; HIGH TEMPERATURE EFFECTS; LUMINESCENCE; OPTIMIZATION; PAINT; REYNOLDS NUMBER; SURFACE ROUGHNESS; TRANSITION FLOW; TRANSONIC AERODYNAMICS;

EID: 1642438244     PISSN: 07302010     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (20)

References (7)
  • 1
    • 85015302972 scopus 로고    scopus 로고
    • ETW-High Quality Test Performance in Cryogenic Environment
    • June
    • J. Quest, "ETW-High Quality Test Performance in Cryogenic Environment", AIAA Paper 00-2206, June 2000.
    • (2000) AIAA Paper , vol.2206
    • Quest, J.1
  • 2
    • 84894359170 scopus 로고    scopus 로고
    • Non-Intrusive Optical Measuring Techniques Operated in Cryogenic Test Conditions at the European Transonic Windtunnel
    • AIAA Paper 99-0946, January
    • D. Ansell, and D. Schimanski, "Non-Intrusive Optical Measuring Techniques Operated in Cryogenic Test Conditions at the European Transonic Windtunnel", AIAA Paper 99-0946, January 1999.
    • (1999) AIAA Paper
    • Ansell, D.1    Schimanski, D.2
  • 3
    • 85006961637 scopus 로고
    • Temperature Sensitive Fluorescent Paint Systems
    • AIAA Paper 94-2483, June
    • Campbell, B. T., Liu, and Sullivan, J. P., "Temperature Sensitive Fluorescent Paint Systems", AIAA Paper 94-2483, June 1994.
    • (1994) AIAA Paper
    • Campbell, B.T.1    Liu2    Sullivan, J.P.3
  • 4
    • 0030786182 scopus 로고    scopus 로고
    • Boundary-Layer Transition Detection in a Cryogenic Wind Tunnel Using Luminescence Paint
    • Jan.-Feb
    • Asai, K., Kanda, H., Kunimasu, T., Liu, T. and Sullivan, J. P., "Boundary-Layer Transition Detection in a Cryogenic Wind Tunnel Using Luminescence Paint", J. of Aircraft, Vol. 34. No.1, Jan.-Feb 1997, see also AIAA Paper 96-2185.
    • (1997) J. of Aircraft , vol.34 , Issue.1
    • Asai, K.1    Kanda, H.2    Kunimasu, T.3    Liu, T.4    Sullivan, J.P.5
  • 5
    • 0030786182 scopus 로고    scopus 로고
    • AIAA Paper 96-2185
    • Asai, K., Kanda, H., Kunimasu, T., Liu, T. and Sullivan, J. P., "Boundary-Layer Transition Detection in a Cryogenic Wind Tunnel Using Luminescence Paint", J. of Aircraft, Vol. 34. No.1, Jan.-Feb 1997, see also AIAA Paper 96-2185.
    • AIAA Paper
  • 6
    • 85069089496 scopus 로고    scopus 로고
    • Optimization of Temperature Sensitive Paint Formulation for Cryogenic Wind Tunnels
    • July (in Japanese)
    • Iijima, Y., Egami, Y., and Asai, K., "Optimization of Temperature Sensitive Paint Formulation for Cryogenic Wind Tunnels", J. Visualization Society of Japan, Vol.22, Suppl. No.1, pp.321-324, July 2002 (in Japanese).
    • (2002) J. Visualization Society of Japan , vol.22 , Issue.SUPPL. 1 , pp. 321-324
    • Iijima, Y.1    Egami, Y.2    Asai, K.3
  • 7
    • 0346179614 scopus 로고
    • Compiled by Tizard J. A., Document ETW/D/95001, February
    • "ETW USER GUIDE", Compiled by Tizard J. A., Document ETW/D/95001, February 1995.
    • (1995) ETW User Guide


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.