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


Personal Author(s) : Bromm, Jr , August F ; O'Donnell, Robert M


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/048258.pdf


Report Date : 17 Dec 1954


Pagination or Media Count : 27


Descriptors :   *EXHAUST NOZZLES , *SUPERSONIC NOZZLES , BODIES OF REVOLUTION , DISTRIBUTION , VELOCITY , PRESSURE


Subject Categories : Fuels
      Jet and Gas Turbine Engines


Distribution Statement : APPROVED FOR PUBLIC RELEASE