Flight Measurements With the Douglas D-558-II (BuAero No. 37974) Research Airplane: Static Longitudinal Stability and Control Characteristics at Mach Numbers Up to 0.87 Page: 1 of 50
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NACA
RESEARCH MEMORANDUM
FLIGHT MEASUREMENTS WITH THE DOUGLAS D-558-11
(BUAERO NO. 37974) RESEARCH AIRPLANE
STATIC LONGITUDINAL STABILITY AND CONTROL CHARACTERISTICS
AT MIACH NUMBERS UP TO 0.87
q By S. A. Sjoberg, James R. Peele,
iflk 1 Irand John H. Griffith
langley Aeronautical LaAtSSYFICATION CHANGE
Langley Field, Va.
UNCLASSIFIED
~ RMa To__
By authority of r'.. Date
CTLS FILED DOCUMENT
Tbus documentt caas ctaisfi e ormn affatag t hetiaonal Dknxes of tM United taes witean ta
mear. i of the Epionage Act, USC 6031 and S. a tracatasin br the r eiltion of its antnLts in any
mtannr to an uaunhartzed person is prohibited by in.
Informatim so claianid way rearted ol to persons la the sltay sat naval services of the United 7
t-qz, appropriate civilian ofleers anS e paya, 4fth lY r GoVcermnot v in legitimate Lnterest
ntorein. and to United&B ste etaoet htsan iIq andL i ere:w w rTbtcnaity must he informed tireof.
NATIONAL ADVISORY COMMITTEE
FOR AERONAUTICS
T WASH NGTON
j.January 17, 1951
COFt DEN TIAL
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Sjoberg, S. A.; Peele, James R. & Griffith, John H. Flight Measurements With the Douglas D-558-II (BuAero No. 37974) Research Airplane: Static Longitudinal Stability and Control Characteristics at Mach Numbers Up to 0.87, report, January 17, 1951; (https://digital.library.unt.edu/ark:/67531/metadc58740/m1/1/: accessed April 19, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.