Investigations on the stability, oscillation, and stress conditions of airplanes with tab control. : First partial report - Derivation of the equations of motion and their general solutions / by B. Filzek.
For the design and the construction of airplanes the control is of special significance, not only with regard to the flight mechhnical properties but also for the proportional arrangement of wing unit, fuselage, and tail unit. whereas these problems may be regarded as solved for direct control of ai...
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| Main Author: | |
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| Corporate Author: | |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Commitee for Aeronautics,
[1949]
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| Series: | Technical memorandum (United States. National Advisory Committee for Aeronautics) ;
no. 1197. |
| Subjects: |
Norlin Library - Basement - Government Information - US
| Call Number: |
Y 3.N 21/5:8/1197
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| Y 3.N 21/5:8/1197 | Available Place a Hold |