Skip to content

Opening book details…

About this scholarly article

20th AIAA Applied Aerodynamics Conference - Computations of Roll-Damping Stability Derivative for Body/Cruciform-Tail Configuration by Huang, Juan-Chen; Lin, Herng; Chieng, Ching-Chang is a scholarly article available to read on EtoBox.

Author
Huang, Juan-Chen; Lin, Herng; Chieng, Ching-Chang
Publisher
American Institute of Aeronautics and Astronautics
Published
2002

More by Huang, Juan-Chen; Lin, Herng; Chieng, Ching-Chang

Browse all works by Huang, Juan-Chen; Lin, Herng; Chieng, Ching-Chang