The present report contains the results thus far obtained and is intended to form the basis of further tests on using the momentum method. The method of testing is presented in detail and the photographs taken during these tests are interpreted.
Measurement of Profile Drag on an Airplane in Flight by the Momentum Method. Part I
1930-03-01
Miscellaneous
No indication
English
Measurement of profile drag on an airplane in flight by the momentum method
Engineering Index Backfile | 1930
|Obtaining airplane drag data from nonsteady flight
AIAA | 1965
|Determination of profile drag of airplane wing in flight at high Reynolds numbers
Engineering Index Backfile | 1939
|Engineering Index Backfile | 1929
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