메뉴 건너뛰기




Volumn , Issue , 2004, Pages 9975-9983

Vortex generators near shock/ boundary layer interactions

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; BOUNDARY LAYERS; DRAG; ERROR ANALYSIS; FLOW VISUALIZATION; REYNOLDS NUMBER; SHOCK WAVES; SUPERSONIC FLOW; VORTEX FLOW;

EID: 2942735333     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-1242     Document Type: Conference Paper
Times cited : (28)

References (24)
  • 1
    • 0023834188 scopus 로고
    • Vortex/ separated boundary layer interactions at transonic mach numbers
    • January
    • Mehta, R., "Vortex/ Separated Boundary Layer Interactions at Transonic Mach Numbers," AIAA Journal, Vol. 26, No. 1, January 1988, pp. 15-26.
    • (1988) AIAA Journal , vol.26 , Issue.1 , pp. 15-26
    • Mehta, R.1
  • 2
    • 0021937157 scopus 로고
    • Shock wave/ turbulent boundary layer interaction and its control
    • Delery, J., "Shock Wave/ Turbulent Boundary Layer Interaction and its Control," Progress in Aerospace Sciences, Vol. 22, No. 4, 1985, pp. 209-280.
    • (1985) Progress in Aerospace Sciences , vol.22 , Issue.4 , pp. 209-280
    • Delery, J.1
  • 3
    • 0025479711 scopus 로고
    • Small submerged vortex generators for turbulent flow separation control
    • Sep-Oct
    • Lin, J., Howard, F., and Selby, G., "Small Submerged Vortex Generators for Turbulent Flow Separation Control," Journal of Spacecraft and Rockets, Vol. 27, No. 5, Sep-Oct 1990, pp. 503-507.
    • (1990) Journal of Spacecraft and Rockets , vol.27 , Issue.5 , pp. 503-507
    • Lin, J.1    Howard, F.2    Selby, G.3
  • 4
    • 0012883268 scopus 로고    scopus 로고
    • A numerical study of the application of vane and air-jet vortex generators
    • May
    • Kupper, C. and Henry, F., "A Numerical Study of the Application of Vane and Air-Jet Vortex Generators," The Aeronautical Journal, No. 2542, May 2001, pp. 255-265.
    • (2001) The Aeronautical Journal , Issue.2542 , pp. 255-265
    • Kupper, C.1    Henry, F.2
  • 5
    • 0000250414 scopus 로고
    • Boundary layer control for aerofoils and wings
    • edited by G. Lachmann, chap. 4, Pergamon Press, Oxford?????, holger has copy?? shelfmark in CUEG library TA78 and TA79
    • Pearcey, H., "Boundary Layer Control for Aerofoils and Wings," Boundary Layer and Flow Control: Its Principles and Application. (2 Volumes), edited by G. Lachmann, chap. 4, Pergamon Press, Oxford?????, 1961, pp. 1261-1333, holger has copy?? shelfmark in CUEG library TA78 and TA79.
    • (1961) Boundary Layer and Flow Control: Its Principles and Application. (2 Volumes) , pp. 1261-1333
    • Pearcey, H.1
  • 6
    • 0029380109 scopus 로고
    • Reduction of fluctuating pressure loads in shock/ boundary-layer interactions
    • Barter, J. W. and Dolling, D. S., "Reduction of Fluctuating Pressure Loads in Shock/ Boundary-Layer Interactions," AIAA Journal, Vol. 33, No. 10, 1995, pp. 1842-1849.
    • (1995) AIAA Journal , vol.33 , Issue.10 , pp. 1842-1849
    • Barter, J.W.1    Dolling, D.S.2
  • 7
    • 0027697022 scopus 로고
    • Vortex control technique for the attenuation of fin buffet
    • November - December
    • Bean, D., Greenwell, D.. and Wood, N., "Vortex Control Technique for the Attenuation of Fin Buffet," Journal of Aircraft, Vol. 30, No. 6, November - December 1993, pp. 847-853.
    • (1993) Journal of Aircraft , vol.30 , Issue.6 , pp. 847-853
    • Bean, D.1    Greenwell, D.2    Wood, N.3
  • 8
    • 33747807866 scopus 로고    scopus 로고
    • Vortex generator installation drag on an airplane near its cruise condition
    • Jan.
    • Kusunose, K. and Yu, N., "Vortex Generator Installation Drag on an Airplane Near Its Cruise Condition," AIAA Paper 03-0932, Jan. 2003.
    • (2003) AIAA Paper , vol.3 , Issue.932
    • Kusunose, K.1    Yu, N.2
  • 9
    • 0028534295 scopus 로고
    • Flow structures in the wake of a wishbone vortex generator
    • November
    • Wendt, B. and Hingst, W., "Flow Structures in the Wake of a Wishbone Vortex Generator," AIAA. Journal, Vol. 32, No. 11, November 1994, pp. 2234-2240.
    • (1994) AIAA. Journal , vol.32 , Issue.11 , pp. 2234-2240
    • Wendt, B.1    Hingst, W.2
  • 10
    • 2942747526 scopus 로고    scopus 로고
    • Research at DERA on sub- boundary layer vortex generators (SBVGs)
    • Jan.
    • Ashill, P., Fulker, J., and Hackett, K., "Research at DERA on Sub- Boundary Layer Vortex Generators (SBVGs)," AIAA Paper 01-0831, Jan. 2001.
    • (2001) AIAA Paper , vol.1 , Issue.831
    • Ashill, P.1    Fulker, J.2    Hackett, K.3
  • 11
    • 0024715515 scopus 로고
    • Computational simulation of vortex generator effects on transonic shock/boundary-layer interaction
    • August
    • Inger, G. and Siebersma, T., "Computational Simulation of Vortex Generator Effects on Transonic Shock/Boundary-Layer Interaction," Journal of Aircraft, Vol. 26, No. 8, August 1989, pp. 697-698.
    • (1989) Journal of Aircraft , vol.26 , Issue.8 , pp. 697-698
    • Inger, G.1    Siebersma, T.2
  • 12
    • 0342951898 scopus 로고
    • Transonic shockwave / turbulent boundary layer interactions on a porous surface
    • May
    • Chokani, N. and Squire, L., "Transonic Shockwave / Turbulent Boundary Layer Interactions on a Porous Surface," Aeronautical Journal, May 1993, pp. 163-170.
    • (1993) Aeronautical Journal , pp. 163-170
    • Chokani, N.1    Squire, L.2
  • 13
    • 0033698843 scopus 로고    scopus 로고
    • Passive control of shock wave - Boundary-layer interactions
    • Gibson, T., Babinsky, H., and Squire, L., "Passive Control of Shock Wave - Boundary-Layer Interactions," Aeronautical Journal, Vol. 104, No. 1033, 2000, pp. 129-140.
    • (2000) Aeronautical Journal , vol.104 , Issue.1033 , pp. 129-140
    • Gibson, T.1    Babinsky, H.2    Squire, L.3
  • 14
    • 0023833712 scopus 로고
    • Passive control of shock boundary layer interaction
    • Raghunathan, S., "Passive Control of Shock Boundary Layer Interaction," Progress in Aerospace Sciences, Vol. 25, No. 3, 1988, pp. 271-296.
    • (1988) Progress in Aerospace Sciences , vol.25 , Issue.3 , pp. 271-296
    • Raghunathan, S.1
  • 15
    • 0343387297 scopus 로고
    • Passive control of transonic shock/ boundary layer interactions
    • IUTAM, Springer-Verlag, Gottingen
    • Thiede, P. and Krogmann, P., "Passive Control of Transonic Shock/ Boundary Layer Interactions," Symposium Transonicum III, IUTAM, Springer-Verlag, Gottingen, 1988, pp. 379-388.
    • (1988) Symposium Transonicum III , pp. 379-388
    • Thiede, P.1    Krogmann, P.2
  • 16
    • 0142169243 scopus 로고    scopus 로고
    • Active control of swept shock wave/ boundary layer interactions
    • University of Cambridge, Department of Engineering
    • Babinsky, H., "Active Control of Swept Shock Wave/ Boundary Layer Interactions," Euroshock II final technical report, University of Cambridge, Department of Engineering, 1999.
    • (1999) Euroshock II Final Technical Report
    • Babinsky, H.1
  • 17
    • 0021853605 scopus 로고
    • Effects of suction on shock/ boundary-layer interaction and shock-induced separation
    • January
    • Krogmann, P., Stanewsky, E., and Thiede, P., "Effects of Suction on Shock/ Boundary-Layer Interaction and Shock-Induced Separation," Journal of Aircraft, Vol. 22, No. 1, January 1985, pp. 37-42.
    • (1985) Journal of Aircraft , vol.22 , Issue.1 , pp. 37-42
    • Krogmann, P.1    Stanewsky, E.2    Thiede, P.3
  • 18
    • 0034357608 scopus 로고    scopus 로고
    • Aerodynamic benefits of adaptive wing technology
    • Stanewsky, E., "Aerodynamic Benefits of Adaptive Wing Technology," Aerospace Science and Technology, Vol. 4, No. 7, 2000. pp. 439-452.
    • (2000) Aerospace Science and Technology , vol.4 , Issue.7 , pp. 439-452
    • Stanewsky, E.1
  • 19
    • 0032759315 scopus 로고    scopus 로고
    • Shock phenomena in high speed aerodynamics: Still a source of major concern
    • January
    • Delery, J., "Shock Phenomena in High Speed Aerodynamics: Still a Source of Major Concern," The Aeronautical Journal, Vol. 103, No. 1019, January 1999, pp. 19-34.
    • (1999) The Aeronautical Journal , vol.103 , Issue.1019 , pp. 19-34
    • Delery, J.1
  • 20
    • 0036744282 scopus 로고    scopus 로고
    • Normal shock wave-turbulent boundary-layer interactions in the presence of streamwise slots and grooves
    • Smith, A., Babinsky, H., Fulker, J., and Ashill, P., "Normal Shock Wave-Turbulent Boundary-Layer Interactions in the Presence of Streamwise Slots and Grooves," The Aeronautical Journal, No. 2628, 2002, pp. 493-500.
    • (2002) The Aeronautical Journal , Issue.2628 , pp. 493-500
    • Smith, A.1    Babinsky, H.2    Fulker, J.3    Ashill, P.4
  • 21
    • 2942753191 scopus 로고    scopus 로고
    • Computational investigation of groove controlled shock wave / boundary layer interaction
    • Jan.
    • Smith, A., Babinsky, H., Dhanasekaran, C., Savill, M., and Dawes, B., "Computational Investigation of Groove Controlled Shock Wave / Boundary Layer Interaction," AIAA Paper 03-0446, Jan. 2003.
    • (2003) AIAA Paper , vol.3 , Issue.446
    • Smith, A.1    Babinsky, H.2    Dhanasekaran, C.3    Savill, M.4    Dawes, B.5
  • 22
    • 2942710755 scopus 로고    scopus 로고
    • Shock / boundary layer interaction control using 3D devices
    • Jan.
    • Holden, H. and Babinsky, H., "Shock / Boundary Layer Interaction Control Using 3D Devices," AIAA Paper 03-0447, Jan. 2003.
    • (2003) AIAA Paper , vol.3 , Issue.447
    • Holden, H.1    Babinsky, H.2
  • 23
    • 35648973110 scopus 로고    scopus 로고
    • Control of normal shock wave / turbulent boundary layer interactions using streamwise grooves
    • Jan.
    • Smith, A. N., Holden, H. A., Babinsky, H., Ashill, P., and Fulker, J., "Control of Normal Shock Wave / Turbulent Boundary Layer Interactions Using Streamwise Grooves," AIAA Paper 02-0978, Jan. 2002.
    • (2002) AIAA Paper , vol.2 , Issue.978
    • Smith, A.N.1    Holden, H.A.2    Babinsky, H.3    Ashill, P.4    Fulker, J.5
  • 24
    • 0026627107 scopus 로고
    • A study of the interaction of a normal shock wave with a turbulent boundary layer at mach numbers between 1.3 and 1.55
    • Atkin, C. and Squire, L., "A Study of the Interaction of a Normal Shock Wave with a Turbulent Boundary Layer at Mach Numbers Between 1.3 and 1.55," European Journal of Mechanics, B Fluids, Vol. 11, No. 1, 1992, pp. 93-118.
    • (1992) European Journal of Mechanics, B Fluids , vol.11 , Issue.1 , pp. 93-118
    • Atkin, C.1    Squire, L.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.