Unsteady Aerodynamic Loads on a UAS Model during a Pitch Maneuver with Roll
Author:
Affiliation:
1. Illinois Institute of Technology
Publisher
American Institute of Aeronautics and Astronautics
Reference6 articles.
1. Dynamic Active Flow Control of the Roll Moment on a Generic UCAS Wing
2. Cook, M. V., Flight Dynamics Principles: A Linear Systems Approach to Aircraft Stability and Control, 3rded., Butterworth-Heinemann,Waltham, MA, 2013, Chap. 2, pp.21, 23.
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