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Parametric Experimental Investigation Of A Scramjet Nozzle At Mach 6 With Freon And Argon Or Air Used For Exhaust Simulation
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Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722905989 Total Pages :108 pages Book Rating :4.9/5 (59 download)
Book Synopsis A Parametric Experimental Investigation of a Scramjet Nozzle at Mach 6 with Freon and Argon Or Air Used for Exhaust Simulation by : National Aeronautics and Space Administration (NASA)
Download or read book A Parametric Experimental Investigation of a Scramjet Nozzle at Mach 6 with Freon and Argon Or Air Used for Exhaust Simulation written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-17 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt: A parametric experimental investigation of a scramjet nozzle was conducted with a gas mixture used to simulate the scramjet engine exhaust flow at a free-stream Reynolds number of approximately 6.5 x 10(exp 6) per foot. External nozzle surface angles of 16, 20, and 24 deg were tested with a fixed-length ramp and for cowl internal surface angles of 6 and 12 deg. Pressure data on the external nozzle surface were obtained for mixtures of Freon and argon gases with a ratio of specific heats of about 1.23, which matches that of a scramjet exhaust. Forces and moments were determined by integration of the pressure data. Two nozzle configurations were also tested with air used to simulate the exhaust flow. On the external nozzle surface, lift and thrust forces for air exhaust simulation were approximately half of those for Freon-argon exhaust simulation and the pitching moment was approximately a third. These differences were primarily due to the difference in the ratios of specific heats between the two exhaust simulation gases. A 20 deg external surface angle produced the greatest thrust for a 6 deg cowl internal surface angle. A flow fence significantly increased lift and thrust forces over those for the nozzle without a flow fence. Cubbage, James M. and Monta, William J. Langley Research Center EXHAUST FLOW SIMULATION; EXHAUST GASES; EXHAUST NOZZLES; FLOW DISTRIBUTION; NOZZLE FLOW; SUPERSONIC COMBUSTION RAMJET ENGINES; ARGON; FREON; GAS FLOW; HYPERSONIC SPEED; LIFT; PITCHING MOMENTS; THRUST...
Book Synopsis Parametric Experimental Investigation of a Scramjet Nozzle at Mach 6 with Freon and Argon Or Air Used for Exhaust Simulation by : James M. Cubbage
Download or read book Parametric Experimental Investigation of a Scramjet Nozzle at Mach 6 with Freon and Argon Or Air Used for Exhaust Simulation written by James M. Cubbage and published by . This book was released on 1991 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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