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Increase in the Maximum Lift of an Airplane Wing Due to a Sudden Increase in Its Effective Angle of Attack Resulting From a Gust
Author:
Kramer, Max
Year:
1932
Document Type:
N/A
Series:
NACA Technical Memorandums
Report Number:
NACA-TM-678
Link:
https://digital.library.unt.edu/ark:/67531/metadc63582/
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