Static Aerodynamic Characteristics at Mach Numbers from 2.50 to 4.63 of a Staged Airplane Model Designed for Cruise Above Mach 5

Static Aerodynamic Characteristics at Mach Numbers from 2.50 to 4.63 of a Staged Airplane Model Designed for Cruise Above Mach 5
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Total Pages : 62
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ISBN-10 : NASA:31769000664030
ISBN-13 :
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Book Synopsis Static Aerodynamic Characteristics at Mach Numbers from 2.50 to 4.63 of a Staged Airplane Model Designed for Cruise Above Mach 5 by :

Download or read book Static Aerodynamic Characteristics at Mach Numbers from 2.50 to 4.63 of a Staged Airplane Model Designed for Cruise Above Mach 5 written by and published by . This book was released on 1964 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt:


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Summary: A flight investigation was made to compare static pressures in subsonic and supersonic flow over an airplane wing as measured by static-pressure tubes,