Analysis of pressure data obtained at transonic speeds on a thin low-aspect-ratio cambered delta wing-body combination
Description:
From Introduction: "Wind-tunnel and flight tests have shown that conical leading-edge camber on a thin low-aspect-ratio delta wing results in increasing the lift-drag ratio at transonic and low supersonic speeds (refs. 1 and 2). References 3 and 4 present the results of two previous investigations of this general program. A more detailed analysis of the pressure distributions of reference 5 is presented herein in terms of total section loads and overall wing-body characteristics."
Date:
September 26, 1958
Creator:
Mugler, John P., Jr.
Item Type:
Refine your search to only
Report