Simulation of unsteady hypersonic combustion around projectiles in an expansion tube
By: S. Yungster and K. Radhakrishnan.
Contributors: Rādhākr̥ṣṇan, Ke.; NASA Glenn Research Center.
Series: [NASA contractor report] -- NASA/CR-1999-209304.; NASA contractor report -- NASA CR-209304.
Publisher: National Aeronautics and Space Administration, Glenn Research Center; National Technical Information Service, distributor
Published: 1999
Place of publication: [Cleveland, Ohio]; Springfield, VA
Language: eng
Format: Microform
Subjects: Computational fluid dynamics.; Unsteady flow.; Projectiles.; Flow distribution.; Hypersonic combustion.
Notes: Shipping list no.: 2000-0307-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1999] 1 microfiche.