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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