SCOPUS 정보 검색 플랫폼

Volumn 23, Issue 4, 1997, Pages 347-352

Vortex breakdown over a delta wing with oscillating leading edge flaps

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0000337443 PISSN: 07234864 EISSN: None Source Type: Journal
DOI: 10.1007/s003480050121 Document Type: Article

Times cited : (17)

References (14)

1
- 3343002327
- AIAA-88-3744
- Cheng HK; Edwards RH; Jia ZX; Lee CJ (1988) Vortex-dominated slender-wing problems studied by a point-vortex method. AIAA-88-3744
- (1988) Vortex-dominated Slender-wing Problems Studied by a Point-vortex Method
- Cheng, H.K.¹ Edwards, R.H.² Jia, Z.X.³ Lee, C.J.⁴

2
- 0030285939
- Effect of leading edge flaps on vortices and vortex breakdown
- Deng Q; Gursul I (1996) Effect of leading edge flaps on vortices and vortex breakdown. J Aircraft 33: 1079-1086
- (1996) J Aircraft , vol.33 , pp. 1079-1086
- Deng, Q.¹ Gursul, I.²

3
- 0028378145
- Unsteady flow phenomena over delta wings at high angle of attack
- Gursul I (1994) Unsteady flow phenomena over delta wings at high angle of attack. AIAA J 32: 225-231
- (1994) AIAA J , vol.32 , pp. 225-231
- Gursul, I.¹

4
- 0028381664
- Vortex breakdown over delta wings in unsteady freestream
- Gursul I; Ho CM (1994) Vortex breakdown over delta wings in unsteady freestream. AIAA J 32: 433-436
- (1994) AIAA J , vol.32 , pp. 433-436
- Gursul, I.¹ Ho, C.M.²

6
- 0021230832
- Aerospace America
- Lamar JE; Campbell JF (1984) Vortex flaps-advanced control devices for supercruise fighters. Aerospace America, pp 95-99
- (1984) Vortex Flaps-advanced Control Devices for Supercruise Fighters , pp. 95-99
- Lamar, J.E.¹ Campbell, J.F.²

7
- 85008267530
- Lift force of delta wings
- Lee M; Ho CM (1990) Lift force of delta wings. Appl Mech Rev 43: 209-221
- (1990) Appl Mech Rev , vol.43 , pp. 209-221
- Lee, M.¹ Ho, C.M.²

8
- 0019664403
- Aerodynamics of inverted leading-edge flaps on delta wings
- Marchman JF (1981) Aerodynamics of inverted leading-edge flaps on delta wings. J Aircraft 18: 1051-1056
- (1981) J Aircraft , vol.18 , pp. 1051-1056
- Marchman, J.F.¹

9
- 0004383163
- NASA CR-159161
- Rao DM (1979) Leading edge vortex flap experiments on a 74 delta flap wing. NASA CR-159161
- (1979) Leading Edge Vortex Flap Experiments on a 74 Delta Flap Wing
- Rao, D.M.¹

10
- 85003260198
- Spanwise pressure distribution on delta wing with leading-edge vortex flap
- Reddy CS (1987) Spanwise pressure distribution on delta wing with leading-edge vortex flap. J Aircraft 24: 222-224
- (1987) J Aircraft , vol.24 , pp. 222-224
- Reddy, C.S.¹

11
- 0003587703
- AIAA Paper 93-0550
- Rockwell D (1993) Three-dimensional flow structure on delta wings at high angle-of-attack: experimental concepts and issues. AIAA Paper 93-0550
- (1993) Three-dimensional Flow Structure on Delta Wings at High Angle-of-attack: Experimental Concepts and Issues
- Rockwell, D.¹

13
- 33845785586
- AIAA Paper 95-0585
- Visbal MR (1995) Computational and physical aspects of vortex breakdown on delta wings. AIAA Paper 95-0585
- (1995) Computational and Physical Aspects of Vortex Breakdown on Delta Wings
- Visbal, M.R.¹

14
- 0030461286
- Multiple-actuator control of vortex breakdown on a pitching delta wing
- Vorobieff P; Rockwell D (1996) Multiple-actuator control of vortex breakdown on a pitching delta wing. AIAA J 34: 2184-2186
- (1996) AIAA J , vol.34 , pp. 2184-2186
- Vorobieff, P.¹ Rockwell, D.²

* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.