Method For Calculating The Rolling And Yawing Moments Due To Rolling For Unswept Wings With Or Without Flaps Or Ailerons By Use Of Nonlinear Section Lift Data
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Method for Calculating the Rolling and Yawing Moments Due to Rolling for Unswept Wings with Or Without Flaps Or Ailerons by Use of Nonlinear Section Lift Data
The methods of NACA Reports 865 and 1090 have been applied to the calculation of the rolling- and yawing-moment coefficients due to rolling for unswept wings with or without flaps or ailerons. The methods allow the use of nonlinear section lift data together with lifting-line theory. Two calculated examples are presented in simplified computing forms in order to illustrate the procedures involved.
Annual Report - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
language: en
Publisher:
Release Date: 1955
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Annual Report
Author: United States. National Advisory Committee for Aeronautics
language: en
Publisher:
Release Date: 1953