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Volumn 22, Issue 1, 1996, Pages 33-44

Non-uniform recovery of vortex breakdown over delta wing in response to blowing along vortex core

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; FLOW VISUALIZATION; LASER DOPPLER VELOCIMETERS; PERTURBATION TECHNIQUES; RECOVERY; SEPARATION; VELOCITY MEASUREMENT; WINGS;

EID: 0030285822     PISSN: 07234864     EISSN: None     Source Type: Journal    
DOI: 10.1007/BF01893304     Document Type: Article
Times cited : (5)

References (18)
  • 1
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    • Leading-edge vortices due to low reynolds number flow past a pitching delta wing
    • Atta R; Rockwell D (1990) Leading-edge vortices due to low reynolds number flow past a pitching delta wing. AIAA J 28(6): 995-1004
    • (1990) AIAA J , vol.28 , Issue.6 , pp. 995-1004
    • Atta, R.1    Rockwell, D.2
  • 2
    • 0016943063 scopus 로고
    • Leading-edge vortex augmentation in compressible flow
    • Bradley RG; Whitten PD; Wray WO (1976) Leading-edge vortex augmentation in compressible flow. J Aircraft 13(9): 238-242
    • (1976) J Aircraft , vol.13 , Issue.9 , pp. 238-242
    • Bradley, R.G.1    Whitten, P.D.2    Wray, W.O.3
  • 3
    • 0016999725 scopus 로고
    • Augmentation of vortex lift by spanwise blowing
    • Campbell JF (1976) Augmentation of vortex lift by spanwise blowing. J Aircraft 13(9): 727-732
    • (1976) J Aircraft , vol.13 , Issue.9 , pp. 727-732
    • Campbell, J.F.1
  • 4
    • 0022709615 scopus 로고
    • Unsteady vortical flow around three dimensional lifting surface
    • Gad-el-Hak M; Ho CM (1986) Unsteady vortical flow around three dimensional lifting surface. AIAA J 24(5): 713-721
    • (1986) AIAA J , vol.24 , Issue.5 , pp. 713-721
    • Gad-el-Hak, M.1    Ho, C.M.2
  • 5
    • 0027623710 scopus 로고
    • Control of vortices on delta wing by leading-edge injection
    • Gu W; Robinson O; Rockwell D (1993) Control of vortices on delta wing by leading-edge injection. AIAA 31(7): 1177-1186
    • (1993) AIAA , vol.31 , Issue.7 , pp. 1177-1186
    • Gu, W.1    Robinson, O.2    Rockwell, D.3
  • 6
    • 0000286943 scopus 로고
    • Vortex breakdown
    • Hall MG (1972) Vortex breakdown. Ann Rev Fluid Mech 4: 195-246
    • (1972) Ann Rev Fluid Mech , vol.4 , pp. 195-246
    • Hall, M.G.1
  • 7
    • 0020782413 scopus 로고
    • Dynamics of aircombat
    • Herbst WB (1983) Dynamics of aircombat. J Aircraft 20(7): 694-598
    • (1983) J Aircraft , vol.20 , Issue.7 , pp. 694-1598
    • Herbst, W.B.1
  • 9
    • 0025383635 scopus 로고
    • Vortex dynamics on a pitching delta wing
    • LeMay SP; Batill SM; Nelson RC (1990) Vortex dynamics on a pitching delta wing. J Aircraft 27(2): 131-138
    • (1990) J Aircraft , vol.27 , Issue.2 , pp. 131-138
    • LeMay, S.P.1    Batill, S.M.2    Nelson, R.C.3
  • 10
    • 0026892950 scopus 로고
    • Non-uniform motion of leading-edge vortex breakdown on ramp pitching delta wings
    • Miau JJ; Chang RC; Chou JH; Lin CK (1992) Non-uniform motion of leading-edge vortex breakdown on ramp pitching delta wings. AIAA J 30(7): 1691-1702
    • (1992) AIAA J , vol.30 , Issue.7 , pp. 1691-1702
    • Miau, J.J.1    Chang, R.C.2    Chou, J.H.3    Lin, C.K.4
  • 11
    • 0023961722 scopus 로고
    • Visualization and wake surveys of vortical flow over a delta wing
    • Payne FM; Ng TT; Nelson RC (1991) Visualization and wake surveys of vortical flow over a delta wing. AIAA J 26(2): 137-143
    • (1991) AIAA J , vol.26 , Issue.2 , pp. 137-143
    • Payne, F.M.1    Ng, T.T.2    Nelson, R.C.3
  • 12
    • 0015039667 scopus 로고
    • Predictions of vortex-lift characteristics by a leading-edge suction analogy
    • Polhamus EC (1971) Predictions of vortex-lift characteristics by a leading-edge suction analogy. J Aircraft 8(4): 193-199
    • (1971) J Aircraft , vol.8 , Issue.4 , pp. 193-199
    • Polhamus, E.C.1
  • 13
    • 0021478885 scopus 로고
    • Applying slender wing benefits to military aircraft
    • Polhamus EC (1984) Applying slender wing benefits to military aircraft. J Aircraft 21(8): 545-559
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  • 18
    • 0015021235 scopus 로고
    • Vortex breakdown on slender sharp-edge wings
    • Wentz WH; Kohliman DL (1971) Vortex breakdown on slender sharp-edge wings. J Aircraft 8(3): 156-161
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.