Unsteady aerodynamics for advanced configurations.
Part V.
Unsteady potential flow around slender bodies at angles of attack /
T.C. Li.

Description

Main Author

Li, T. C.

Related Names

United States. Air Force.
Air Force Flight Dynamics Laboratory (U.S.)
North American Aviation. Space and Information Systems Division

Language(s)

English

Published

Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965.

Subjects

Nonlinear systems.
Aerodynamics > Aerodynamics / Mathematical models.
Flutter (Aerodynamics)
Unsteady flow (Aerodynamics)

Physical Description

viii, 42 pages : illustrations, figures ; 28 cm.

Locate a Print Version

Find in a library

Viewability