Euler technology assessment for preliminary aircraft design
Subtitle: unstructured/structured grid NASTD application for aerodynamic analysis of an advanced fighter/tailless configuration
By: Todd R. Michal.
Contributors: Langley Research Center.; United States. National Aeronautics and Space Administration.
Series: NASA/CR -- 1998-206947; NASA contractor report -- NASA CR-206947.
Publisher: National Aeronautics and Space Administration, Langley Research Center; Available from the National Technical Information Service
Published: 1998
Place of publication: Hampton, Va; Springfield, VA
Language: eng
Format: Microform
Subjects: Computational fluid dynamics.; Euler equations of motion.; Aircraft design.; Cambered wings.; Controllability.; Directional control.; Fighter aircraft.; Navier-Stokes equation.; Sideslip.; Tailless aircraft.
Notes: Shipping list no.: 99-0388-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1998] 1 microfiche.