The Effect of an Operating Propeller on the Aerodynamic Characteristics at High Subsonic Speeds of a Model of a Vertical-Rising Airplane Having an Unswept Wing of Aspect Ratio 3 Page: 1 of 91
This report is part of the collection entitled: National Advisory Committee for Aeronautics Collection and was provided to Digital Library by the UNT Libraries Government Documents Department.
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THE EFFECT OF AN OPERATING PROPELLER ON THE AERODYNAMIC
CHARACTERISTICS AT HIGH SUBSONIC SPEEDS OF A MODEL.. -
OF A VERTICAL-RISING AIRPLANE HAVING AN UNSWEPT ._.
WING OF ASPECT RATIO 3
By Fred B. Sutton and Donald A. Buell
Ames Aeronautical Laboratory - .
Moffett Field, Calif.
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manner to an p r is proldisted by law.
NATIONAL ADVISORY COMMITTEE
- November 15, 1954
CON FIDE TIAL
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Sutton, Fred B. & Buell, Donald A. The Effect of an Operating Propeller on the Aerodynamic Characteristics at High Subsonic Speeds of a Model of a Vertical-Rising Airplane Having an Unswept Wing of Aspect Ratio 3, report, November 15, 1954; (https://digital.library.unt.edu/ark:/67531/metadc59185/m1/1/?rotate=270: accessed May 20, 2019), University of North Texas Libraries, Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.