Euler technology assessment for preliminary aircraft design - compressibility predictions by employing the Cartesian unstructured grid SPLITFLOW code
By: Dennis B. Finley and Steve L. Karman.
Contributors: Karman, Steve L.; Langley Research Center
Publisher: Langley Research Center
Published: 1996
Place of publication: Hampton, Va
Number of pages: 94
Subjects: Aircraft design; Compressible flow; Computational grids; Euler equations of motion
Notes: Includes bibliographical references.