Accession Number:

AD0294335

Title:

UNSTEADY SUPERSONIC FLOW OVER A CONE WITH A BLUNTED TIP

Descriptive Note:

Corporate Author:

GRUMMAN AIRCRAFT ENGINEERING CORP BETHPAGE NY

Personal Author(s):

Report Date:

1962-12-01

Pagination or Media Count:

28.0

Abstract:

Subject Categories:

  • Theoretical Mathematics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE