Estimation of the maximum angle of sideslip for determination of vertical-tail loads in rolling maneuvers /
This paper presents the results of a study, by a step-by-step integration of the equations of motion, of the variations of angle of sideslip and angle of attack in rolling maneuvers, particularly for airplanes with mass distributed mainly along the fuselage. The results are compared with those of ex...
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| Corporate Authors: | , |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1952
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
2633 |
| Subjects: |
Internet
This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.Stanford University
| Call Number: |
NACA TN 2633 |
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