An investigaion of boattail geometry and Reynolds number effects on forebody and afterbody drag at transonic Mach numbers /
A.V. Spratley.

APA Citation

Spratley, A. V.., United States. Air Force. Systems Command., Arnold Engineering Development Center., ARO, I. (1977). An investigaion of boattail geometry and Reynolds number effects on forebody and afterbody drag at transonic Mach numbers. Arnold Air Force Base, Tennessee: Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force.

MLA Citation

Spratley, A. V., United States. Air Force. Systems Command, Arnold Engineering Development Center, and Inc. ARO. An Investigaion of Boattail Geometry And Reynolds Number Effects On Forebody And Afterbody Drag At Transonic Mach Numbers. Arnold Air Force Base, Tennessee: Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1977.

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