Euler technology assessment
Subtitle: SPLITFLOW code applications for stability and control analysis on an advanced fighter model employing innovative control concepts
By: Keith J. Jordan.
Contributors: Langley Research Center.; United States. National Aeronautics and Space Administration.
Series: [NASA contractor report] -- NASA/CR-1998-206943.; NASA contractor report -- NASA CR-206943.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1998
Place of publication: Hampton, Va; Springfield, VA
Language: eng
Format: Microform
Subjects: Computational fluid dynamics.; Unstructured grids (Mathematics); Aerodynamic stability.; Angle of attack.; Fighter aircraft.; Viscous flow.; Turbulent flow.; Finite volume method.; Navier-Stokes equation.; Inviscid flow.
Other titles: SPLITFLOW code applications for stability and control analysis on an advanced fighter model employing innovative control concepts.
Notes: Shipping list no.: 99-0631-M.

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