Unsteady aerodynamics for advanced configurations. Part V. Unsteady potential flow around slender bodies at angles of attack - Li, T. C.; United States. Air Force. Systems Command; Air Force Flight Dynamics Laboratory (U.S.); North American Aviation. Space and Information Systems Division (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965)
Includes bibliograpical references (page 42).
Air Force Contract No.
Mode of access: Internet.
Keywords: Nonlinear systems; Aerodynamics -- Mathematical models; Flutter (Aerodynamics); Unsteady flow (Aerodynamics)