Equations of motion for airplane penetrating gust derived using few simplifying assumptions; calculations of loads for different static longitudinal stability on two German airplane models, HC 45 and HS 122, compared with flight tests. English translation from (ZWB) Forschungsbericht n 1422 Dec 31 1940.
Influence of static longitudinal stability on behavior of airplanes in gusts
NACA -- Tech Memo
National Advisory Committee for Aeronautics -- Technical Memorandums ; Tech Memo 1323
1951
26 pages
Report
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Static longitudinal stability of "Ente" airplanes
NTRS | 1931
|Static longitudinal stability of "Ente" airplanes
TIBKAT | 1931
|Static longitudinal stability of "Ente" airplanes
Engineering Index Backfile | 1930
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