Accession Number : ADA956519

Title :   Experimental Investigation of a 10 degrees Conical Turbojet Plug Nozzle with Translating Primary and Secondary Shrouds at Mach Numbers from 0 to 2.0.

Descriptive Note : Technical memo.,

Corporate Author : NATIONAL AERONAUTICS AND SPACE ADMINISTRATION CLEVELAND OH LEWIS RESEARCH CEN TER

Personal Author(s) : Bresnahan, Donald L.

Report Date : APR 1969

Pagination or Media Count : 36

Descriptors :   *TURBOJET EXHAUST NOZZLES, *TURBOJET ENGINES, *SUPERSONIC FLIGHT, AIR BREATHING ENGINES, MACH NUMBER, AERODYNAMIC CHARACTERISTICS, SUPERSONIC WIND TUNNELS, AFTERBURNING.

Subject Categories : Jet and Gas Turbine Engines
      Aerodynamics

Distribution Statement : APPROVED FOR PUBLIC RELEASE