Investigation of the Effect of a Nacelle at Various Chordwise and Vertical Positions on the Aerodynamic Characteristics at High Subsonic Speeds of a 45 Degrees Sweptback Wing With and Without a Fuselage Page: 1 of 73
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CQ INFIDENTIAt, :inCop
F .
RESEARCH MEMORANDUM
INVESTIGATION OF THE EFFECT OF A NACELLE AT
VARIOUS CHORDWISE AND VERTICAL POSITIONS ON THE AERODYNAMIIC
CHARACTERISTICS AT HIGH SUBSONIC SPEEDS OF A 450 SWEPTBACK
WING WITH AND WITHOUT A FUSELAGE
By H.I Norman Silvers, Thomas J. King, fr., and
Thomas B. Pasteur, Jr.
Langley Aeronautical Laboratory
i. ASSWIATION CANC J Field, Va.
FOR REFERENCE
thn riyt L _LSA S~ -Date -J2 S wr
CLAIMED DOCUMOEF
This document r ca I lasisted inrmaton asctung ti Nm inanl Defnse of the Unit tatas wita tshe
nmntr g ofi the Espioge Act, USC 50:31 nd 32. Is trnsmsaloa or the revelation of its contents in any
mnnr to an mauthorised person is prohitted by Isw.
Information so clasaifed may be impartsd only to person in the military and naval services of the United h
States, appropriate c yivlan oficers and employees of the Fderal Oaernt who hav a legitimate Interest
therein, and i United States citizens of Iwn loyalty and discretion who of necessity mst beo informed thereof.
NATIONAL ADVISORY COMMITTEE
FOR AERONAUTICS
WASHINGTON
September 24, 1951
LONFI DENIAL
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Silvers, H. Norman; King, Thomas J., Jr. & Pasteur, Thomas B., Jr. Investigation of the Effect of a Nacelle at Various Chordwise and Vertical Positions on the Aerodynamic Characteristics at High Subsonic Speeds of a 45 Degrees Sweptback Wing With and Without a Fuselage, report, September 24, 1951; (https://digital.library.unt.edu/ark:/67531/metadc59052/m1/1/: accessed April 18, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.