Accession Number : AD0435470


Title :   EXPANSIVE FLOW TABLES PERTINENT TO JET FLOW CALCULATIONS


Corporate Author : ARO INC ARNOLD AFS TN


Personal Author(s) : Lyons, S C


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/435470.pdf


Report Date : Apr 1964


Pagination or Media Count : 315


Abstract : Charts and tables are presented for determining approximate values of the initial turning angles and the boundary shapes of jets exhausting to low ambient temperatures. The tables have been compiled to facilitate calculations pertaining to jet flow for various ratios of specific heats from 1.10 to 1.667 and Mach numbers from 1.0000 to 100.00. The ratios p/p sub t and A/A at the nozzle throat and the Prandtl-Meyer angle are given for each Mach number and ratio of specific heats.


Descriptors :   *JET FLOW , *EXHAUST GASES , TABLES(DATA) , ROCKET NOZZLES , SPECIFIC HEAT , HIGH ALTITUDE , PRESSURE


Subject Categories : Fluid Mechanics
      Combustion and Ignition


Distribution Statement : APPROVED FOR PUBLIC RELEASE