Experimental program for real gas flow code validation at NASA Ames Research Center

Original publisher: Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; Springfield, Va. : For sale by the National Technical Information Service, [1989] OCLC Number: (OCoLC)25307391 Subject: Gas flow. Excerpt: ... 21-13 TEST SECTION VACUUM DRIVEN TUBE * CHAMBER-CAPACITOR-DRIVER I I ( 10 ' ) I I _j ( 14 ' ) ( 38 ' ) I I ( 3 0 i n. I I I I I I I I EXIT I I I I I DIA. ) ! I ! ! LOADING VALVE MAIN COLLECTOR MODEL SUPPORT THRUST STAND NOZZLE RING ' Y DIAPHRAGM DIAPHRAGM SPOOL 14 Figure Schematic of Elecmc Arc-Shock Tube ( EAST ) Facility. DRIVEN DRIVER DRIVEN DRIVER GAS DRIVER GAS TUEE.cm DRIVER GAS 1UEE.cm GAS AIR CONICAL 0 He 10 30-in. AIR He v 10 AIR CONICAL A60 He 30-in. AIR 060 He AIR CONICAL 54-in. 0 N2 10 H 2 H 2 10 0 10 He Ar CONICAL A CONICAL H2 10 H 2 0 0 He C02 CONICAL 10 %-in. He A 10 Kr 54-in. AIR D He 10 %-in. He H2INe IO n AIR CONICAL 0 H2 10-lo4 atm = P5 500 ( AIR. 4 "-TUBE )-103-102 c g-10 &-w ' a 3 3 l-a. K-10-1-10-2 11.000 22,000 I