Charts of Normal Shock Wave Properties in Imperfect Air

This report has yet to be scanned by Contrails staff

Report Number: AEDC TDR 64-43
Author(s): Lewis, Clark H., Burgess, E. G., III
Corporate Author(s): ARO, Inc.
Date of Publication: 1964-03
Pages: 46
Contract: AF 40(600)-1000
DoD Project: None Given
Identifier: AD0433958

Abstract:
Gas-dynamic properties which include the effects of dissociation, ionization, and intermolecular forces (van der Walls) are presented for incident and reflected shock waves in equilibrium imperfect air. Charts are presented for incident shock Mach numbers in the range from 6 to 30 into (ideal) air at a temperature of 300 K and pressures in the range from 10 to the minus 4 power to 10 to the 3rd power cm Hg. The temperature and density in any region do not exceed, respectively, 15,000 K and 158 amagats. In addition to the usual incident and reflected shock properties, stagnation conditions upstream and downstream and conditions immediately downstream of a standing shock wave are also presented. At pressures above one atmosphere in the undisturbed gas, the effects of the intermolecular forces on the gas-dynamic properties are demonstrated.

Provenance: IIT

Other options for obtaining this report:

Via the Defense Technical Information Center (DTIC):
A record for this report, and possibly a pdf download of the report, exists at DTIC

Via National Technical Report Library:
This report may be available for download from NTRL. Use the Title from this record to locate the item in DTIC Online

Indications of Public Availability
No digital image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement



Export