On the effect of subsonic trailing edges on damping in roll and pitch of thin sweptback wings in a supersonic stream / Herbert S. Ribner.
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1950.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
2146. |
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| Abstract: | The principal effect of subsonic trailing edges on the damping in roll and pitch of thin sweptback wings in a supersonic stream is evaluated in the form of approximate correction terms. These terms are to be added to the corresponding expressions obtained when the trailing-edge disturbances are ignored. Application is limited to plan forms and Mach numbers for which the trailing-edge disturbance does not extend beyond the leading edge and for which the area of mutual tip-trailing-edge interference is not large. |
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| Item Description: | "August 1950." NACA TN Number 2146. |
| Physical Description: | 27 pages : illustrations ; 28 cm. |
| Bibliography: | Includes bibliographical references. |
| Action Note: | committed to retain |