Aerodynamic Flow Control using a Variable Droop Leading Edge Airfoil

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Chandrasekhara_Aerodynamic_Flow_2004.pdf (1.26 MB)
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Tung, C.
Martin, P.B.
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Specialists Meeting (RSM) on ﾓEnhancement of Military Flight Vehicle Performance by Management of Interacting Boundary Layer Transition and Separationﾔ, RTO-MP-AVT-111; www.rti.nato.int, Prague, Czech Republic, Oct. 4-7, 2004.
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Chandrasekhara, M.S., Tung, C., and Martin, P.B., ﾓAerodynamic Flow Control using a Variable Droop Leading Edge Airfoilﾔ, Specialists Meeting (RSM) on ﾓEnhancement of Military Flight Vehicle Performance by Management of Interacting Boundary Layer Transition and Separationﾔ, RTO-MP-AVT-111; www.rti.nato.int, Prague, Czech Republic, Oct. 4-7, 2004.
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This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.
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