Accession Number : AD0479694


Title :   A THEORETICAL PERFORMANCE INVESTIGATION OF AN AFTERBURNING TURBOFAN ENGINE. APPENDIX


Descriptive Note : Master's thesis


Corporate Author : NAVAL POSTGRADUATE SCHOOL MONTEREY CA


Personal Author(s) : Bell, James F


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/479694.pdf


Report Date : Jan 1962


Pagination or Media Count : 184


Descriptors :   *TURBOFAN ENGINES , AFTERBURNERS , COMPRESSORS , COMPUTER PROGRAMMING , DIFFUSERS , DIGITAL COMPUTERS , FUEL CONSUMPTION , GAS TURBINES , HIGH ALTITUDE , JET TRANSPORT AIRCRAFT , PERFORMANCE(ENGINEERING) , PROGRAMMING LANGUAGES , SUPERSONIC AIRCRAFT , SUPERSONIC FLIGHT , TABLES(DATA) , THEORY , THRUST , TURBOJET ENGINES , TURBOJET EXHAUST NOZZLES , TURBORAMJET ENGINES


Subject Categories : Jet and Gas Turbine Engines


Distribution Statement : APPROVED FOR PUBLIC RELEASE