Accession Number:

AD0684453

Title:

ON THE NON-LINEAR PROPAGATION OF SHOCK WAVES THROUGH NON-UNIFORM INCOMING FLOWS,

Descriptive Note:

Corporate Author:

BOEING SCIENTIFIC RESEARCH LABS SEATTLE WASH FLIGHT SCIENCES LAB

Personal Author(s):

Report Date:

1968-12-01

Pagination or Media Count:

56.0

Abstract:

The general problem studied is the propagation of an oblique shock wave through a two-dimensional steady non-uniform oncoming flow. Author

Subject Categories:

  • Fluid Mechanics
  • Radiofrequency Wave Propagation

Distribution Statement:

APPROVED FOR PUBLIC RELEASE