Measured and predicted section wave drag coefficients at a Mach number of 1.6 for a delta wing with two airfoil sections /

Bibliographic Details
Main Authors: Grant, Frederick C (Frederick Clifton), 1891-1974, Grant, Frederick C
Corporate Author: Langley Research Center
Format: Book
Language:English
Published: Washington, [D.C.] : National Aeronautics and Space Administration, 1959
Series:NASA technical note ; D-11
NASA technical note ; D-11
Subjects:

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Stanford University

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Call Number: NASA TN D-11

Yale University

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Call Number: NASA TN D-11