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Volume 17, Issue 7
1 July 1945
This article was originally published in
Aircraft Engineering
Aircraft Engineering Cover Image for Volume 17, Issue 7
Review Article| July 01 1945

Wing Pitching Moment Coefficient

W.L. Morse, B.Sc. (Eng.), A.M.I.Mech. E., A.F.R.Ae.S.
W.L. Morse, B.Sc. (Eng.), A.M.I.Mech. E., A.F.R.Ae.S.
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Author & Article Information
Publisher: Emerald Publishing
Online ISSN: 2059-9366
Print ISSN: 0002-2667
© MCB UP Limited
1945
Aircraft Engineering (1945) 17 (7): 204–205.
https://doi.org/10.1108/eb031266

SCHRENK'S method for finding the wing lift distribution which has already been given in AIRCRAFT ENGINEERING can be taken further in order to determine the Pitching Moment Coefficient, CM0, about the quarter‐chord point of the mean chord at no‐lift.

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© MCB UP Limited
1945
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