A flight investigation of the effect of center-of-gravity location on gust loads / Jack Funk and Earle T. Binckley.

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Bibliographic Details
Main Author: Funk, Jack N.
Corporate Author: United States. National Advisory Committee for Aeronautics
Other Authors: Binckley, Earle T.
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1951.
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 2575.
Subjects:

MARC

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245 1 2 |a A flight investigation of the effect of center-of-gravity location on gust loads /  |c Jack Funk and Earle T. Binckley. 
260 |a Washington, D.C. :  |b National Advisory Committee for Aeronautics,  |c 1951. 
300 |a 18 pages :  |b illustrations ;  |c 28 cm. 
336 |a text  |b txt  |2 rdacontent. 
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490 1 |a National Advisory Committee for Aeronautics ;  |v no. 2575. 
500 |a "December 1951." 
500 |a NACA TN Number 2575. 
504 |a Includes bibliographical references. 
520 3 |a Two jet-propeleed airplanes were flown in rough air to investigate the effects of center-of-gravity location on gust loads. Data wer obtained at centers of gravity of 20.9 and 27.5 percent mean aerodynamic chord for incremental load factor up to 1 g. The results indicat that a 6.6-percent forward movement of center of gravity decreases the gust loads by approximately 10 percent. The most frequently occuring distance from 1 g to peak acceleration was 17.5 chords. Calculations of the change in normal acceleration for a center-of-gravity movement from 20.9 to 27.5 percent mean aerodynamic chord for a single triangular gust having a gradient distance of 17.5 chords were in good agreement with the test results. 
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650 0 |a Gust loads.  |0 http://id.loc.gov/authorities/subjects/sh85057991. 
650 0 |a Center of mass.  |0 http://id.loc.gov/authorities/subjects/sh85021847. 
650 0 |a Stability of airplanes, Longitudinal.  |0 http://id.loc.gov/authorities/subjects/sh85127188. 
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650 7 |a Gust loads.  |2 fast  |0 (OCoLC)fst00949518. 
650 7 |a Stability of airplanes, Longitudinal.  |2 fast  |0 (OCoLC)fst01131217. 
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