Note on an application of the tilting plate method of Mach number variation for wind tunnel tests at low supersonic speeds
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Author
Contributions
- Haverty, L. - Contributor
- Aeronautical Research Council (Great Britain) - Contributor
- Royal Aircraft Establishment (Great Britain) - Contributor
Publication
1953 - Ministry of Supply, Aeronautical Research Council, London
Subjects
Series Statement
- Royal Aircraft Establishment. Technical note -- no. Aero 2238
- Aeronautical Research Council. Current papers -- no. 168
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