Determination by the Free-Fall Method of the Drag and Longitudinal Stability and Control Characteristics of a Canard Model at Transonic Speeds Page: 1 of 47
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^RESEARCH MEMORANDUM
DETERMINATION BY THE FREE -FALL ME THOD OF TEE DRAG AND
LONGITUDINAL STABILITY AND C ONTROL C HARAC TERISTICS
OF A CANARD MODEL AT TRANS ONIC SPEEDS
By Christopher C. Kraft, Jr. and Charles W. Mathews
Langley Aeronautical Laboratory
Langley Air Force Base, Va.
2SS1FCAT 1' CANCELLED
1 4 &a t arS -- .4 . . A.: m. t elon ! 2e0t n a
tEater itt i the meantrkg o the Btepage Act,
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- irmatwi n Iosatiead may be Imparted
titsh4 $. p2h*r--a n e in the mul_ ary ani -sal
-errtes of the United S&stes, apprprlate
slrin oficers mad employees of LM Federal
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NATIONAL ADVISORY COMMITTEE
FOR AERONAUTICS
WASHINGTON
August 25, 1950 UNCLASSIFIED
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Kraft, Christopher C., Jr. & Mathews, Charles W. Determination by the Free-Fall Method of the Drag and Longitudinal Stability and Control Characteristics of a Canard Model at Transonic Speeds, report, August 25, 1950; (https://digital.library.unt.edu/ark:/67531/metadc58452/m1/1/: accessed May 14, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.