메뉴 건너뛰기




Volumn 3, Issue , 2007, Pages 1944-1964

The second International Vortex Flow Experiment (VFE-2): Objectives and present status

Author keywords

[No Author keywords available]

Indexed keywords

MEASUREMENT THEORY; NUMERICAL METHODS; TURBULENCE MODELS; VORTEX FLOW; WIND TUNNELS;

EID: 35648969988     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-4446     Document Type: Conference Paper
Times cited : (10)

References (30)
  • 1
    • 4444312882 scopus 로고
    • The International Vortex Flow Experiment for Computer Code Validation
    • Drougge, G., " The International Vortex Flow Experiment for Computer Code Validation," ICAS-Proceedings Jerusalem 1988, Vol. 1, pp. XXXV-XLI.
    • (1988) ICAS-Proceedings Jerusalem , vol.1
    • Drougge, G.1
  • 4
    • 78149452571 scopus 로고
    • Modelling and Numerical Simulation of Vortex Flow in Aerodynamics
    • to
    • Hoeijmakers, H. W. M., "Modelling and Numerical Simulation of Vortex Flow in Aerodynamics," AGARD-CP 494, 1991, pp. 1-1 to 1-46.
    • (1991) AGARD-CP , vol.494
    • Hoeijmakers, H.W.M.1
  • 6
    • 2942714253 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
  • 8
    • 0345592699 scopus 로고
    • Experimentelle Untersuchung der Strömung auf der Saugseite eines Schlanken Deltaflügels
    • Hummel, D., "Experimentelle Untersuchung der Strömung auf der Saugseite eines Schlanken Deltaflügels," Z. Flugwiss. 13, 1965, 247-252.
    • (1965) Z. Flugwiss , vol.13 , pp. 247-252
    • Hummel, D.1
  • 10
    • 0003870549 scopus 로고    scopus 로고
    • Computed Unsteady Structure of Spiral Vortex Breakdown on Delta Wings
    • AIAA Paper 96-2074
    • Visbal, M. R., "Computed Unsteady Structure of Spiral Vortex Breakdown on Delta Wings," AIAA Paper 96-2074, 1996.
    • (1996)
    • Visbal, M.R.1
  • 11
    • 35648970952 scopus 로고    scopus 로고
    • Numerical Analysis of the Unsteady Flow Above a Slender Delta Wing at Large Angles of Attack
    • Paper ICA0252
    • Müller, J., and Hummel, D., "Numerical Analysis of the Unsteady Flow Above a Slender Delta Wing at Large Angles of Attack," ICAS Proceedings Harrogate 2000, Paper ICA0252, 2000.
    • (2000) ICAS Proceedings Harrogate 2000
    • Müller, J.1    Hummel, D.2
  • 12
    • 2642580139 scopus 로고    scopus 로고
    • A Review of Steps Taken to Create an International Virtual Laboratory at NASA Langley for Aerodynamic Prediction and Comparison
    • Lamar, J. E., Cronin, C. K., and Scott, L. E., "A Review of Steps Taken to Create an International Virtual Laboratory at NASA Langley for Aerodynamic Prediction and Comparison," Progress in Aerospace Sciences, Vol. 40, 2004, pp. 163 - 172.
    • (2004) Progress in Aerospace Sciences , vol.40 , pp. 163-172
    • Lamar, J.E.1    Cronin, C.K.2    Scott, L.E.3
  • 16
    • 2942715250 scopus 로고    scopus 로고
    • Luckring, J. M., Compressibility and Leading-Edge Bluntness Effects for a 65° Delta Wing. AIAA Paper 2004-0765, 2004.
    • Luckring, J. M., "Compressibility and Leading-Edge Bluntness Effects for a 65° Delta Wing. AIAA Paper 2004-0765, 2004.
  • 17
    • 78149428493 scopus 로고    scopus 로고
    • Reynolds Number, Compressibility, and Leading-Edge Bluntness Effects on Delta-Wing Aerodynamics
    • Paper 4.1.4
    • Luckring, J. M., "Reynolds Number, Compressibility, and Leading-Edge Bluntness Effects on Delta-Wing Aerodynamics," ICAS Proceedings Yokohama 2004, Paper 4.1.4, 2004.
    • (2004) ICAS Proceedings Yokohama 2004
    • Luckring, J.M.1
  • 18
    • 85081478868 scopus 로고    scopus 로고
    • 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.
    • 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.
  • 20
    • 33845416121 scopus 로고    scopus 로고
    • Application of Stereo-PIV to the VFE-2 65° Delta Wing Configuration at Sub- and Transonic Speeds
    • AIAA Paper 2006-3486
    • Schröder, A., Agocs, J., Frahnert, H., Otter, D., Mattner, H., Kompenhans, J., and Konrath, R., "Application of Stereo-PIV to the VFE-2 65° Delta Wing Configuration at Sub- and Transonic Speeds." AIAA Paper 2006-3486, 2006.
    • (2006)
    • Schröder, A.1    Agocs, J.2    Frahnert, H.3    Otter, D.4    Mattner, H.5    Kompenhans, J.6    Konrath, R.7
  • 21
    • 35648965103 scopus 로고    scopus 로고
    • Analysis of PIV Results Obtained for the VFE-2 65° Delta Wing Configuration at Sub- and Transonic Speeds
    • AIAA Paper 2006-3003
    • Konrath, R., Schröder, A., and 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)
    • Konrath, R.1    Schröder, A.2    Kompenhans, J.3
  • 22
    • 33947577697 scopus 로고    scopus 로고
    • nd International Symposium Integrating CFD and Experiments in Aerodynamics, 5-6 September 2005, Cranfield University, UK, J. Aerospace Engineering, 220, 2006, Nr. 6, pp. 559 - 568.
    • nd International Symposium Integrating CFD and Experiments in Aerodynamics, 5-6 September 2005, Cranfield University, UK, J. Aerospace Engineering, Vol.. 220, 2006, Nr. 6, pp. 559 - 568.
  • 23
    • 85081475325 scopus 로고    scopus 로고
    • Konrath, R., Klein, Ch., Schroeder, A., and Kompenhans, J., Combined Application of Pressure Sensitive Paint and Particle Image Velocimetry to the Flow Above a Delta Wing. 12th International Symposium on Flow Visualization, Sept. 10 - 14, 2006, DLR Goettingen, Germany, In Grant, I. [Ed.]: CD Rom Proceedings (ISFV12-67.2), Optimage Ltd., Edinburgh, UK, pp. 1 - 14.
    • Konrath, R., Klein, Ch., Schroeder, A., and Kompenhans, J., "Combined Application of Pressure Sensitive Paint and Particle Image Velocimetry to the Flow Above a Delta Wing. 12th International Symposium on Flow Visualization, Sept. 10 - 14, 2006, DLR Goettingen, Germany, In Grant, I. [Ed.]: CD Rom Proceedings (ISFV12-67.2), Optimage Ltd., Edinburgh, UK, pp. 1 - 14.
  • 24
    • 33846286845 scopus 로고    scopus 로고
    • The Year in Review: Aerodynamic Measurement Technology
    • December
    • Sheplak, M., "The Year in Review: Aerodynamic Measurement Technology." Aerospace America, December 2006, p. 22.
    • (2006) Aerospace America , pp. 22
    • Sheplak, M.1
  • 25
    • 33845409766 scopus 로고    scopus 로고
    • Numerical Investigation of Reynolds Number Effects on a Blunt Leading-Edge Delta Wing
    • AIAA Paper 2006-3001
    • Crippa, S., and Rizzi, A., "Numerical Investigation of Reynolds Number Effects on a Blunt Leading-Edge Delta Wing. AIAA Paper 2006-3001 (2006).
    • (2006)
    • Crippa, S.1    Rizzi, A.2
  • 27
    • 84888713072 scopus 로고    scopus 로고
    • Steady CFD Analysis of Delta Wing Vortex Flow with Means of Structured Multiblock RANS-Solver NSMB in the International Vortex Flow Experiment-2
    • Bartussek, U., "Steady CFD Analysis of Delta Wing Vortex Flow with Means of Structured Multiblock RANS-Solver NSMB in the International Vortex Flow Experiment-2." ICAS Proceedings Hamburg 2006.
    • ICAS Proceedings Hamburg 2006
    • Bartussek, U.1
  • 28
    • 84888668159 scopus 로고    scopus 로고
    • Initial Steady/Unsteady CFD Analysis of Vortex Flow Over the VFE-2 Delta Wing
    • Paper P2.18
    • Crippa, S., and Rizzi, A., "Initial Steady/Unsteady CFD Analysis of Vortex Flow Over the VFE-2 Delta Wing." ICAS Proceedings Hamburg 2006, Paper P2.18.
    • ICAS Proceedings Hamburg 2006
    • Crippa, S.1    Rizzi, A.2
  • 29
    • 33845438089 scopus 로고    scopus 로고
    • Analysis of Transonic Flow on a Slender Delta Wing Using CFD
    • AIAA Paper 2006-3171
    • Schiavetta, L. A., Boelens, O. J., and Fritz, W., "Analysis of Transonic Flow on a Slender Delta Wing Using CFD," AIAA Paper 2006-3171,2006.
    • (2006)
    • Schiavetta, L.A.1    Boelens, O.J.2    Fritz, W.3
  • 30
    • 34250796728 scopus 로고    scopus 로고
    • Comparison of DES and URANS for Unsteady Vortical Flows Over Delta Wings
    • AIAA Paper 2007-1085
    • Schiavetta, L. A., Badcock, K., and Cummings, R., "Comparison of DES and URANS for Unsteady Vortical Flows Over Delta Wings." AIAA Paper 2007-1085 (2007).
    • (2007)
    • Schiavetta, L.A.1    Badcock, K.2    Cummings, R.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.