Wind tunnel tests on slotted flaps on a low wing monoplane: flap angle 0 to 90 degrees
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Author
Contributions
- Morgan, M. B. - Contributor
- Aeronautical Research Committee (Great Britain) - Contributor
Publication
1936 - Aeronautical Research Committee, London
Subjects
Series Statement
- Aeronautical Research Committee. Reports and memoranda -- no. 1735
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