A study of the effects of Reynolds number and Mach number on constant pressure coefficient jump for shock-induced trailing-edge separation
By: Atlee M. Cunningham and Gregory S. Spragle.
Contributors: Spragle, Gregory S.; General Dynamics Corporation; Langley Research Center
Publisher: Langley Research Center
Published: 1987
Place of publication: Hampton, Va
Number of pages: 79
Subjects: Mach number; Reynolds number; Trailing edges; Transonic flow
Notes: Bibliographical references: p.28-31.

Contract number: NAS1-17955