Approximate method for calculating motions in angles of attack and sideslip due to step pitching- and yawing-moment inputs during steady roll / Martin T. Moul and Teresa R. Brennan.
Saved in:
| Main Author: | |
|---|---|
| Corporate Author: | |
| Other Authors: | |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington :
National Advisory Committee for Aeronautics,
[1958]
|
| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
4346. |
| Subjects: |
| Abstract: | The simplified method of NACA Report 1344 for calculating motions in angles of attack and sideslip resulting from a trim angle of attack and steady rolling velocity has been extended in the present paper to the condition of pitching- yawing-moment inputs. The resulting formulas are intended primarily for rolling-velocity conditions in which rolling divergence is not encountered. From the calculated angles of attack and sideslip, preliminary estimates of aircraft loads for design purposes can be made. Motions calculated with the simplified method are compared with exact solutions of the five-dgree-of freedom equations. |
|---|---|
| Item Description: | "September 1958." NACA TN Number 4346. |
| Physical Description: | 42 pages : illustrations ; 27 cm. |
| Bibliography: | Includes bibliographical references. |
| Action Note: | committed to retain 20230101 20480101 Alliance Shared Trust https://www.coalliance.org/shared-print-archiving-policies. |