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Volumn 3, Issue , 2006, Pages 1882-1893

Application of stereo PIV to the VFE-2 65° delta wing configuration at sub- and transonic speeds

Author keywords

[No Author keywords available]

Indexed keywords

LASER BEAMS; PRESSURE MEASUREMENT; STEREO VISION; TRANSONIC FLOW; WIND TUNNELS; WINGS;

EID: 33845416121     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-3486     Document Type: Conference Paper
Times cited : (14)

References (11)
  • 1
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    • A new vortex flow experiment for computer code validation
    • Loen, Norway, 7-11 May 2001, Meeting Proceedings RTO-MP-069 (I), SYA 8-1 to 8-31
    • Hummel, D., and Redeker, G., "A new vortex flow experiment for computer code validation," RTO AVT Symposium on Vortex Flow and High Angle of Attack Aerodynamics, Loen, Norway, 7-11 May 2001, Meeting Proceedings RTO-MP-069 (I), SYA 8-1 to 8-31, 2003
    • (2003) RTO AVT Symposium on Vortex Flow and High Angle of Attack Aerodynamics
    • Hummel, D.1    Redeker, G.2
  • 3
    • 0012314391 scopus 로고    scopus 로고
    • Experimental surface pressure data obtained on 65° delta wing across Reynolds number and Mach number ranges
    • Chu, J., and Luckring, J.M., "Experimental surface pressure data obtained on 65° delta wing across Reynolds number and Mach number ranges," NASA TM 4645, 1996
    • (1996) NASA TM , vol.4645
    • Chu, J.1    Luckring, J.M.2
  • 4
    • 33845444295 scopus 로고    scopus 로고
    • Development of PSP technique for application on the VFE-2 65° delta wing configuration in sub- And transonic flow
    • Klein, C., Sachs, W., Henne, U., Engler, R.H., Wiedemann, A. and Konrath, R., "Development of PSP technique for application on the VFE-2 65° delta wing configuration in sub- and transonic flow," AIAA-Paper 2006-0059, 2006
    • (2006) AIAA-Paper , vol.2006 , Issue.59
    • Klein, C.1    Sachs, W.2    Henne, U.3    Engler, R.H.4    Wiedemann, A.5    Konrath, R.6
  • 5
    • 34250759802 scopus 로고    scopus 로고
    • Analysis of PSP results obtained for the VFE-2 65° delta wing configuration at sub- And transonic speed
    • Konrath, R., Klein, C., Engler, R.H., Otter, D., "Analysis of PSP Results Obtained for the VFE-2 65° Delta Wing Configuration at Sub- and Transonic Speed," AIAA-Paper 2006-0060, 2006
    • (2006) AIAA-Paper , vol.2006 , Issue.60
    • Konrath, R.1    Klein, C.2    Engler, R.H.3    Otter, D.4
  • 8
    • 0036921706 scopus 로고    scopus 로고
    • Generation and control of tracer particles for optical flow investigations in air
    • Kähler, C., Sammler, B., Kompenhans, J.," Generation and control of tracer particles for optical flow investigations in air" Experiments in Fluids, 33, 6, S. 736-742, 2002
    • (2002) Experiments in Fluids , vol.33 , Issue.6 , pp. 736-742
    • Kähler, C.1    Sammler, B.2    Kompenhans, J.3
  • 9
    • 0031354164 scopus 로고    scopus 로고
    • Stereoscopic digital particle image velocimetry for application in wind tunnel flows
    • Willert C., "Stereoscopic digital particle image velocimetry for application in wind tunnel flows" Meas. Sci. Technol. 8 1465-79, 1997
    • (1997) Meas. Sci. Technol. , vol.8 , pp. 1465-1479
    • Willert, C.1
  • 10
    • 0036144446 scopus 로고    scopus 로고
    • Iterative image deformation methods in PIV
    • Scarano, F., "Iterative image deformation methods in PIV" Meas. Sci. Technol. 13 (2002) R1-R19
    • (2002) Meas. Sci. Technol. , vol.13
    • Scarano, F.1
  • 11
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    • Analysis of PIV results obtained for the VFE-2 65° delta wing configuration at sub- And transonic speeds
    • Konrath, R., Schröder, A., Kompenhans, J., "Analysis of PIV Results Obtained for the VFE-2 65° Delta Wing Configuration at Sub- and Transonic Speeds," AIAA-Paper 2006-3003, 2006
    • (2006) AIAA-Paper , vol.2006 , Issue.3003
    • Konrath, R.1    Schröder, A.2    Kompenhans, J.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.