Effect of body-mounted lateral controls and speed brakes on the aerodynamic load distribution over a 45 degree swept wing at mach numbers from 0.80 to 0.98 /

Bibliographic Details
Main Author: West, F. E
Corporate Author: United States National Aeronautics and Space Administration
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]
Series:NASA technical note ; D-522
Subjects:

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Stanford University

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Call Number: NASA TN D-522

Yale University

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Call Number: NASA TN D-522