An investigation of hypersonic shock tunnel testing at an equilibrium interface condition of 4,100K: theory and experiment
By: Marco A. S. Minucci and Henry T. Nagamatsu.
Contributors: Nagamatsu, Henry T.; AIAA
Publisher: American Institute of Aeronautics and Astronautics
Published: 1991
Place of publication: Washington, D. C
Number of pages: 17
Subjects: Hypersonic flow; Hypersonic shock tubes
Notes: Includes bibliographical references: p. 11-12.

Source: AIAA 22nd Fluid Dynamics, Plasma Dynamics & Lasers Conference, June 24-26, 1991/Honolulu, Hawaii