Experimental and Theoretical Studies of Interference Effects on the Damping in Roll of the Bell X-1A Research Airplane at Supersonic Speeds (Including Canopy Shape Effects) Page: 1 of 36
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RM L56G27
A, A I3 1176 00051358
RESEARCH MEMORANDUM
EXPERIMENTAL AND THEORE TICAL STUDIES OF INTERFERENCE
EFFECTS ON THE DAMPING IN ROLL OF THE BELL X-lA
RESEARCH AIRPLANE AT SUPERSONIC SPEEDS
(INCLUDING CANOPY SHAPE EFFECTS)
By Russell W. McDearmon and William B. Boatright
CLn,_ASSI FI CA gr .le er aal Laboratory
UN LaSS F ED I
To .- -- - ....OCT 19 1956
LANGLEY AEROI'ITIcA LABORATO!
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by uthno -ty 1 ...... CLASSIFIED DOCU "ENT
" Thi2sma2 tisa teral contai s informationaffecting the National Defense. 'othe United Stateswithln tihe meaning
of the espionage 'laws, TitleS1 U.S.C; Se s' 793 and 794, the transmissian or revelati of which in any a.
/ p manner t oan unauthorized peron is p ohibited by law,; O' " , ,o'ee i w Ine.n e a e, e--" 1
NATIONAL ADVISORY COMMITTEE
FOR AERONAUTICS
WASHINGTON
October 15, 195614I}
CONFi DE I4TIAL
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McDearmon, Russell W. & Boatright, William B. Experimental and Theoretical Studies of Interference Effects on the Damping in Roll of the Bell X-1A Research Airplane at Supersonic Speeds (Including Canopy Shape Effects), report, October 15, 1956; (https://digital.library.unt.edu/ark:/67531/metadc63118/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.