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Volumn , Issue , 2001, Pages

Low speed tests using PSP at Onera

Author keywords

[No Author keywords available]

Indexed keywords

CALIBRATION METHOD; DEGRADATION RATE; DELTA WINGS; FINAL PRESSURE; LOW SPEED; MAXIMAL ERROR; PEUGEOT; PRESSURE TAPS;

EID: 84897876278     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (9)

References (18)
  • 3
    • 0343119279 scopus 로고    scopus 로고
    • First Results Using the New DLR PSP System - Intensity and Lifetime Measurements
    • 14-16 April, Cambridge, UK, Paper 43
    • Engler R.H., Klein C., First Results Using the New DLR PSP System - Intensity and Lifetime Measurements, Wind Tunnels and Wind Tunnel Test Techniques, 14-16 April 1997, Cambridge, UK, Paper 43
    • (1997) Wind Tunnels and Wind Tunnel Test Techniques
    • Engler, R.H.1    Klein, C.2
  • 6
    • 85087594914 scopus 로고    scopus 로고
    • Application of Pressure Sensitive Paint for Determining Aerodynamic Loads on a Scale of the F-16C
    • Paper AIAA 2000-2528, June
    • Sellers M.E., Application of Pressure Sensitive Paint for Determining Aerodynamic Loads on a Scale of the F-16C, 21st AIAA Aerodynamic Measurement Technology and Ground Testing Conference, Paper AIAA 2000-2528, June 2000.
    • (2000) 21st AIAA Aerodynamic Measurement Technology and Ground Testing Conference
    • Sellers, M.E.1
  • 8
    • 0003316189 scopus 로고    scopus 로고
    • Comparison of Pressure Sensitive Paints on a Supercritical Wing at Cruise Speed
    • Edinburgh, UK, paper 207
    • Mebarki Y., Grenier M., Thain J., Comparison of Pressure Sensitive Paints on a Supercritical Wing at Cruise Speed, 9th Intenational Symposium on Flow Visualization, Edinburgh, UK, 2000, paper 207.
    • (2000) 9th Intenational Symposium On Flow Visualization
    • Mebarki, Y.1    Grenier, M.2    Thain, J.3
  • 9
    • 85088722239 scopus 로고    scopus 로고
    • Simultaneous Global Pressure and Temperature Measurement Technique for Hypersonic Wind Tunnels
    • AIAA 2000-2649, June
    • Buck G.M., Simultaneous Global Pressure and Temperature Measurement Technique for Hypersonic Wind Tunnels, 21st AIAA Aerodynamic Measurement Technology and Ground Testing Conference, AIAA 2000-2649, June 2000.
    • (2000) 21st AIAA Aerodynamic Measurement Technology and Ground Testing Conference
    • Buck, G.M.1
  • 14
    • 0346936170 scopus 로고    scopus 로고
    • Low-Speed Flow Studies Using the Pressure Sensitive Paint Technique
    • Brown O.C., Metha R.D., Cantwell B.J., Low-Speed Flow Studies Using the Pressure Sensitive Paint Technique, 81st AGARD/EDP, 1997.
    • (1997) 81st AGARD/EDP
    • Brown, O.C.1    Metha, R.D.2    Cantwell, B.J.3
  • 16
    • 0033278745 scopus 로고    scopus 로고
    • Automatic Registration of Luminescent Paint Images
    • Albuquerque, NM, 1999. Instrumentation Society of America, Research Triangle Park, NC
    • Ruyten W., Automatic Registration of Luminescent Paint Images, 45th International Instrumentation Symposium, Albuquerque, NM, 1999. Instrumentation Society of America, Research Triangle Park, NC, 1999, pp. 279-288.
    • (1999) 45th International Instrumentation Symposium , pp. 279-288
    • Ruyten, W.1
  • 17
    • 0342918679 scopus 로고    scopus 로고
    • Vortical Flow Field Investigation Using a Two-Component Pressure Sensitive Paint at Low Speed
    • Toulouse, France
    • Merienne M.C., Bouvier F., Vortical Flow Field Investigation Using a Two-Component Pressure Sensitive Paint at Low Speed, 18th ICIASF, Toulouse, France, 1999.
    • (1999) 18th ICIASF
    • Merienne, M.C.1    Bouvier, F.2
  • 18
    • 85088721772 scopus 로고    scopus 로고
    • On the Effects of Reflected Light in Luminescent Paint Measurements
    • AIAA-2000-0833, January
    • Ruyten W, Fisher C., On the Effects of Reflected Light in Luminescent Paint Measurements, 38th Aerospace Sciences Meeting and Exhibit, AIAA-2000-0833, January 2000.
    • (2000) 38th Aerospace Sciences Meeting and Exhibit
    • Ruyten, W.1    Fisher, C.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.