Accession Number:

AD0048258

Title:

Investigation at Supersonic Speeds of the Effect of Jet Mach Number and Divergence Angle of the Nozzle upon the Pressure of the Base Annulus of a Body of Revolution

Descriptive Note:

Research memo.

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA

Report Date:

1954-12-17

Pagination or Media Count:

27.0

Abstract:

Subject Categories:

  • Fuels
  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE