Theoretical/numerical study of feasibility of use of winglets on low aspect ratio wings at subsonic and transonic Mach numbers to reduce drag - Info and Reading Options
By John M. Kuhlman
“Theoretical/numerical study of feasibility of use of winglets on low aspect ratio wings at subsonic and transonic Mach numbers to reduce drag” Metadata:
- Title: ➤ Theoretical/numerical study of feasibility of use of winglets on low aspect ratio wings at subsonic and transonic Mach numbers to reduce drag
- Author: John M. Kuhlman
“Theoretical/numerical study of feasibility of use of winglets on low aspect ratio wings at subsonic and transonic Mach numbers to reduce drag” Subjects and Themes:
- Subjects: Drag (Aerodynamics) - Transonic Aerodynamics
Edition Identifiers:
- The Open Library ID: OL7099219W
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