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Volumn , Issue , 2001, Pages

Development of advanced optical instrumentation for use in the NASA Glenn Icing Research Tunnel

Author keywords

[No Author keywords available]

Indexed keywords

FEASIBILITY STUDIES; LIQUID WATER CONTENT; OPTICAL INSTRUMENTATION; PRESSURE SENSITIVE PAINTS; RECONSTRUCTION SOFTWARE; SURFACE CONDITIONS; TIME-RESOLVED METHODS; VIRTUAL INSTRUMENT;

EID: 84897898820     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (4)

References (9)
  • 3
    • 85088760437 scopus 로고    scopus 로고
    • Application of Pressure-Sensitive Paint to Ice Accreted Wind Tunnel Models
    • AIAA Paper 2000-0834, Reno, NV, January 10-13
    • th Aerospace Sciences Meeting, Reno, NV, January 10-13, 2000.
    • (2000) th Aerospace Sciences Meeting
    • Bencic, T.J.1
  • 4
    • 84897905024 scopus 로고    scopus 로고
    • Calibration of Detection Angle for Full-Field Pressure-Sensitive Paint Measurements
    • AIAA Paper 2001-0307, Reno, NV, January 8-11
    • th Aerospace Sciences Meeting, Reno, NV, January 8-11, 2001.
    • (2001) th Aerospace Sciences Meeting
    • Bencic, T.J.1
  • 8
    • 84897870660 scopus 로고    scopus 로고
    • Progress in Measuring Water Impingement Characteristics on Aircraft Surfaces
    • Papadakis, M., Vu, G., Hung, K.E., Bidwell, C.S., Bencic, T.J., Breer, M.D., AIAA 98-0488, Reno, NV
    • th Aerospace Sciences Meeting, Reno, NV, 1998.
    • (1998) th Aerospace Sciences Meeting


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.