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Drag divergence Mach number
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1	MACH NUMBER, RELATIVE THICKNESS, SWEEP AND LIFT COEFFICIENT OF THE WING – AN EMPIRICAL INVESTIGATION OF PARAMETERS AND EQUATIONS D. Scholz, S. Ciornei Hamburg University of Applied Sciences Department of Automotive and Add to Reading List Source URL: www.fzt.haw-hamburg.de Language: English - Date: 2005-10-26 05:29:51 Fluid mechanics Drag divergence Mach number Airfoil Supercritical airfoil Drag Lift Pressure coefficient Camber Mach number Aerodynamics Aerospace engineering Fluid dynamics
2	Mach Number, Relative Thickness, Luftund Sweep andDeutscher Lift Coefficient of the Wing Add to Reading List Source URL: www.fzt.haw-hamburg.de Language: English - Date: 2005-10-26 05:29:08 Fluid mechanics Drag divergence Mach number Drag Critical Mach number Airfoil Swept wing Mach number Lift Wave drag Aerodynamics Aerospace engineering Fluid dynamics
3	TF-8A Crusader with Supercritical Wing NASA Conference Publication[removed]Justin Murtha, John Stephens, Add to Reading List Source URL: www.logbookmag.com Language: English - Date: 2012-02-24 02:11:55 Fluid mechanics Supercritical airfoil Wave drag Transonic speed Airfoil Area rule Drag Wing Drag divergence Mach number Aerodynamics Aerospace engineering Fluid dynamics
4	NASA Technical Paper Add to Reading List Source URL: www.southampton.ac.uk Language: English - Date: 2006-12-04 07:30:46 Fluid mechanics Supercritical airfoil Airfoil Drag divergence Mach number Shock wave Wave drag Lift Pressure coefficient Foil Aerodynamics Aerospace engineering Fluid dynamics

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