Lift and Drag Characteristics of the Bell X-5 Research Airplane at 59 Degrees Sweepback for Mach Numbers from 0.60 to 1.03 Page: 1 of 38
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SECURITY INFC
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RESEARCH MEMORANDUM
LIFT AND DRAG CHARACTERISTICS OF THE BELL X-5 RESEARCH
AIRPLANE AT 590 SWEEPBACK FOR MACH NUMBERS
FROM 0.60 TO 1.03
By Donald R. Bellman
Langley Aeronautical Laboratory
Langley Field, Va.
CLASSIFICATION CHANGED TO UNCASSIPIED
AUTHORITY sNAOA RESEARCH ABSTRACT NO, b7
DATE: FgWWOLrNTI956 Wa
Restiiion/C a ssfiatio n Cance led g the National Defense of the United States within the meaning
s. 793 and 794, the transmission or revelation of which in any
manner to an unauthorized person is prohibited by law.
NATIONAL ADVISORY COMMITTEE
FOR AERONAUTICS
WASHINGTON
February 17, 1953ION
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Bellman, Donald R. Lift and Drag Characteristics of the Bell X-5 Research Airplane at 59 Degrees Sweepback for Mach Numbers from 0.60 to 1.03, report, February 17, 1953; (https://digital.library.unt.edu/ark:/67531/metadc59530/m1/1/: accessed March 29, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.