Measurements of the effects of finite span on the pressure distribution over double-wedge wings at Mach numbers near shock attachment Page: 1 of 51
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NATIONAL ADVISORY COMMITTEE -
TECHNICAL NOTE 3522
MEASUREMENTS OF THE EFFECTS OF FINITE SPAN ON THE
f PRESSURE DISTRIBUTION OVER DOUBLE-WEDGE WINGS
& AT MACH NUMBERS NEAR SHOCK ATTACHMENT
By Walter G. Vincenti
Ames Aeronautical Laboratory
Moffett Field, Calif.
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Vincenti, Walter G. Measurements of the effects of finite span on the pressure distribution over double-wedge wings at Mach numbers near shock attachment, report, September 1955; (digital.library.unt.edu/ark:/67531/metadc57614/m1/1/: accessed February 17, 2019), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.