Euler technology assessment for preliminary aircraft design

unstructured/structured grid NASTD application for aerodynamic analysis of an advanced fighter/tailless configuration

By Todd R. Michal

0 (0 Ratings)

0 Want to read0 Currently reading0 Have read

Publish Date

1998

Publisher

National Aeronautics and Space Administration, Langley Research Center,Available from the National Technical Information Service

Language

eng

Pages

Description:

subjects: Computational fluid dynamics, Controllability, Aircraft design, Navier-Stokes equation, Euler equations of motion, Tailless aircraft, Cambered wings, Sideslip, Directional control, Fighter aircraft