Investigation at supersonic speed (M = 1.53) of the pressure distribution over a 63 degrees swept airfoil of biconvex section at zero lift Page: 1 of 35
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INVESTIGATION AT SUPERSONIC SPEED (M = 1.53) OF TE PRESSIBRE
DISMIBUTION OVER A 630 SWEPT AIRFOIL OF
BICONVEX SECTION AT ZERO IJ P
By Charle W. PFrick and John W. Boyd
Ames Aeronautical Laboratory
Moffett Field, Calif.
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NATIONAL ADVISORY COMMITTEE
June 10, 1948 UNCLASSIFIED)
N AC A LIBRARY
LANGLEY MEMORIAL AE u NAUTIA
Langlke Field. Va
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RM No. A8C22
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Frick, Charles W. & Boyd, John W. Investigation at supersonic speed (M = 1.53) of the pressure distribution over a 63 degrees swept airfoil of biconvex section at zero lift, report, June 10, 1948; (digital.library.unt.edu/ark:/67531/metadc57586/m1/1/: accessed January 19, 2019), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.