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Pseudosteady-state analysis of nonlinear aircraft maneuvers
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Johnson, K. G. Young, J. W. Schy, A. A. |
| Copyright Year | 1980 |
| Description | An analytical method was developed for studying the combined effects of rotational coupling and nonlinear aerodynamics on aircraft response for specified control inputs. The method involves the simultaneous solution of two nonlinear equations which are functions of angle attack, roll rate, and control inputs. The method was applied to a number of maneuvers for a fighter-type aircraft. Time history responses verified the usefulness of the analysis for predicting a variety of response characteristics caused by interacting nonlinear aerodynamic and inertial effects, including spin conditions. |
| File Size | 1986858 |
| Page Count | 65 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19810004554 |
| Archival Resource Key | ark:/13960/t9770965p |
| Language | English |
| Publisher Date | 1980-12-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Stability And Control Flight Characteristics Nonlinear Equations Aircraft Maneuvers Angle of Attack Approach Control Aerodynamic Characteristics Fighter Aircraft Aerodynamic Stalling Prediction Analysis Techniques Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
