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Volumn 15, Issue 6, 2004, Pages 1079-1089

Stereoscopic PIV measurements of leading edge separation vortices on a cranked arrow wing

Author keywords

Fluid flow velocity; Low speed flow; Separation vortex; Stereoscopic PIV

Indexed keywords

ANGLE OF ATTACK INDICATORS; BOUNDARY LAYERS; CORRELATION METHODS; KINETIC ENERGY; REYNOLDS NUMBER; TURBULENCE; VORTEX FLOW; WIND TUNNELS;

EID: 2942652702     PISSN: 09570233     EISSN: None     Source Type: Journal    
DOI: 10.1088/0957-0233/15/6/006     Document Type: Article
Times cited : (19)

References (13)
  • 1
    • 0020259618 scopus 로고
    • Vortex formation over double-delta wings
    • Seattle, US, Aug. 1982
    • Brennenstuhl U and Hummel D 1982 Vortex formation over double-delta wings ICAS paper 82-6.6.3 Seattle, US, Aug. 1982
    • (1982) ICAS Paper 82-6.6.3
    • Brennenstuhl, U.1    Hummel, D.2
  • 2
    • 0012574236 scopus 로고    scopus 로고
    • Reynolds number effects on the vonical-flow structure generated by a double-delta wing
    • Hebbar S K et al 2000 Reynolds number effects on the vonical-flow structure generated by a double-delta wing Exp. Fluids 28 206-16
    • (2000) Exp. Fluids , vol.28 , pp. 206-216
    • Hebbar, S.K.1
  • 3
    • 0002676907 scopus 로고
    • On the vortex formation over a slender wing at large angles of incidence
    • AGARD CP-247, paper no 15
    • Hummel D 1979 On the vortex formation over a slender wing at large angles of incidence High Angle of Attack Aerodynamics AGARD CP-247, paper no 15
    • (1979) High Angle of Attack Aerodynamics
    • Hummel, D.1
  • 5
    • 85034735683 scopus 로고    scopus 로고
    • Aerodynamic characteristics of rolled SST configuration with LE and TE flaps at high angles of attack
    • (Orlando, FL, June 2003) AIAA paper 2003-3413
    • Kwak D-Y et al 2003 Aerodynamic characteristics of rolled SST configuration with LE and TE flaps at high angles of attack 33rd Fluid Dynaimcs Conf. and Exhibit (Oilando, FL, June 2003) AIAA paper 2003-3413
    • (2003) 33rd Fluid Dynaimcs Conf. and Exhibit
    • Kwak, D.-Y.1
  • 6
    • 85034748160 scopus 로고    scopus 로고
    • Analysis of flows over a SST wing-body configuration at low speed and high angles of attack
    • (Orlando, FL, June 2003) AIAA paper 2003-3415
    • Lei Z et al 2003 Analysis of flows over a SST wing-body configuration at low speed and high angles of attack 33rd Fluid Dynamics Conf. and Exhibit (Orlando, FL, June 2003) AIAA paper 2003-3415
    • (2003) 33rd Fluid Dynamics Conf. and Exhibit
    • Lei, Z.1
  • 7
    • 78549272651 scopus 로고    scopus 로고
    • Reynolds number and leading-edge bluntness effects on a 65 delta wing
    • (Reno, Jan. 2002) AIAA paper 2002-0419
    • Luckring J M 2002 Reynolds number and leading-edge bluntness effects on a 65 delta wing 40th Aerospace Sciences Meeting and Exhibit (Reno, Jan. 2002) AIAA paper 2002-0419
    • (2002) 40th Aerospace Sciences Meeting and Exhibit
    • Luckring, J.M.1
  • 11
    • 0036873015 scopus 로고    scopus 로고
    • Effects of Reynolds number on flow over 76/40-degree double-delta wings
    • Verhaagen N G 2002 Effects of Reynolds number on flow over 76/40-degree double-delta wings J. Aircraft 39 1045-52
    • (2002) J. Aircraft , vol.39 , pp. 1045-1052
    • Verhaagen, N.G.1
  • 12
    • 85088755846 scopus 로고    scopus 로고
    • Stereo PIV applications to large-scale low-speed wind tunnels
    • (Reno. Jan. 2003) AIAA paper 2003-0919
    • Watanabe S and Kato H 2003 Stereo PIV applications to large-scale low-speed wind tunnels 41st Aerospace Sciences Meeting and Exhibit (Reno. Jan. 2003) AIAA paper 2003-0919
    • (2003) 41st Aerospace Sciences Meeting and Exhibit
    • Watanabe, S.1    Kato, H.2
  • 13
    • 2942669010 scopus 로고    scopus 로고
    • Aerodynamic design technology of scaled supersonic experiment airplane
    • in Japanese
    • Yoshida K 2001 Aerodynamic design technology of scaled supersonic experiment airplane Proc. 2001 Meeting of Japan Society of Fluid Mechanics pp 561-2 (in Japanese)
    • (2001) Proc. 2001 Meeting of Japan Society of Fluid Mechanics , pp. 561-562
    • Yoshida, K.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.