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Volumn , Issue , 2001, Pages

Active control of separation on a wing with conformal camber

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AEROSPACE ENGINEERING; ANGLE OF ATTACK; REYNOLDS NUMBER; WIND TUNNELS;

EID: 85087595507     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-293     Document Type: Conference Paper
Times cited : (30)

References (30)
  • 5
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    • Separation Control at Flight Reynolds Numbers: Lessons Learned and Future Directions
    • AIAA 2000-2542, Denver, Colorado
    • Seifert, A. and Pack, L. G. "Separation Control at Flight Reynolds Numbers: Lessons Learned and Future Directions, " Fluids 2000, AIAA 2000-2542, Denver, Colorado, 2000.
    • (2000) Fluids 2000
    • Seifert, A.1    Pack, L.G.2
  • 6
    • 2942734620 scopus 로고    scopus 로고
    • Some New Observations Affecting the Control of Separation by Periodic Excitation
    • AIAA 2000-2314, Denver, Colorado
    • Wygnanski, I., "Some New Observations Affecting the Control of Separation by Periodic Excitation, " Fluids 2000, AIAA 2000-2314, Denver, Colorado, 2000.
    • (2000) Fluids 2000
    • Wygnanski, I.1
  • 7
    • 0003281016 scopus 로고    scopus 로고
    • Aerodynamic Control Using Synthetic Jets
    • AIAA 2000-2401, Denver, Colorado
    • Honohan, A. M., Amitay, M., and Glezer, A., "Aerodynamic Control Using Synthetic Jets, " Fluids 2000, AIAA 2000-2401, Denver, Colorado, 2000.
    • (2000) Fluids 2000
    • Honohan, A.M.1    Amitay, M.2    Glezer, A.3
  • 8
    • 2942740353 scopus 로고    scopus 로고
    • Circulation Control Pneumatic Aerodynamics: Blown Force and Moment Augmentation and Modification; Past, Present, and Future
    • AIAA 2000-2541, Denver, Colorado
    • Englar, R. J., "Circulation Control Pneumatic Aerodynamics: Blown Force and Moment Augmentation and Modification; Past, Present, and Future, " Fluids 2000, AIAA 2000-2541, Denver, Colorado, 2000.
    • (2000) Fluids 2000
    • Englar, R.J.1
  • 9
    • 28844449063 scopus 로고    scopus 로고
    • On the Moving Surface Bounday-Layer Control
    • AIAA 2000-2238, Denver, Colorado
    • Modi, V. J., "On the Moving Surface Bounday-Layer Control, " Fluids 2000, AIAA 2000-2238, Denver, Colorado, 2000.
    • (2000) Fluids 2000
    • Modi, V.J.1
  • 14
    • 0029696613 scopus 로고    scopus 로고
    • Integrated Structural Tailoring and Control Using Adaptive Materials for Advanced Aircraft Wings
    • January-February
    • Librescu, L. Meirovitch, L. and Song, O., "Integrated Structural Tailoring and Control Using Adaptive Materials for Advanced Aircraft Wings, " Journal of Aircraft, Vol. 33, No. 1 (January-February 1996), pp. 203-213.
    • (1996) Journal of Aircraft , vol.33 , Issue.1 , pp. 203-213
    • Librescu, L.1    Meirovitch, L.2    Song, O.3
  • 20
    • 0030172890 scopus 로고    scopus 로고
    • Aeroelastic Analysis of a Flexible Airfoil with a Freeplay Non-linearity
    • Kim, S.-H. and Lee, I., "Aeroelastic Analysis of a Flexible Airfoil with a Freeplay Non-linearity, " Journal of Sound and Vibration, 193(4): 823-846, 1996.
    • (1996) Journal of Sound and Vibration , vol.193 , Issue.4 , pp. 823-846
    • Kim, S.-H.1    Lee, I.2
  • 22
    • 0031167769 scopus 로고    scopus 로고
    • Design of a smart material actuator for rotor control
    • Straub, F. K. and Merkley, D. J., "Design of a smart material actuator for rotor control, " Smart Materials and Structures, 6: 26-34, 1997.
    • (1997) Smart Materials and Structures , vol.6 , pp. 26-34
    • Straub, F.K.1    Merkley, D.J.2
  • 28
    • 0019384212 scopus 로고
    • Visualization of Transition in the Flow Over an Airfoil Using the Smoke Wire Technique
    • S. Batill and T. Mueller. "Visualization of Transition in the Flow Over an Airfoil Using the Smoke Wire Technique. " AIAA Journal, 19, 340-345, 1981.
    • (1981) AIAA Journal , vol.19 , pp. 340-345
    • Batill, S.1    Mueller, T.2
  • 30
    • 0344005388 scopus 로고
    • XFOIL: An Analysis and Design System for Low Reynolds Number Airfoils
    • Springer-Verlag
    • Drela, M., "XFOIL: An Analysis and Design System for Low Reynolds Number Airfoils, " Low Reynolds Number Aerodynamics, Springer-Verlag, 1993.
    • (1993) Low Reynolds Number Aerodynamics
    • Drela, M.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.