Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation
By: Lawrence D. Huebner, Marc W. Kniskern and William J. Monta.
Contributors: Kniskern, Marc W.; Monta, William J.; Langley Research Center
Publisher: Langley Research Center
Published: 1993
Place of publication: Hampton, Va
Number of pages: 46
Subjects: Hypersonic wind tunnels; Supersonic combustion ramjet engines
Notes: Includes bibliographical references: p. 10.