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Approximate method for calculating motions in angles of attack and sideslip due to step pitching- and yawing-moment inputs during steady roll
| Content Provider | University of North Texas |
|---|---|
| Author | Moul, Martin T. Brennan, Teresa R. |
| Organization | Langley Aeronautical Laboratory |
| Description | Report presenting an extension of a method for calculating motions in angles of attack and sideslip resulting from a trim angle of attack and steady rolling velocity to the condition of pitching- and yawing-moment inputs. The resulting formulas are intended primarily for rolling-velocity conditions in which rolling divergence is not encountered. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc57209 |
| Language | English |
| Publisher Date | 2018-04-24 |
| Access Restriction | Open |
| Subject Keyword | aerodynamics rolling characteristics |
| Content Type | Text |
| Resource Type | Report |