Cavity Unsteady-Pressure Measurements at Subsonic and Transonic Speeds

Cavity Unsteady-Pressure Measurements at Subsonic and Transonic Speeds
Title Cavity Unsteady-Pressure Measurements at Subsonic and Transonic Speeds PDF eBook
Author Maureen B. Tracy
Publisher
Pages 84
Release 1997
Genre Aerodynamics, Transonic
ISBN

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Characterization of Cavity Flow Fields Using Pressure Data Obtained in the Langley 0.3-Meter Transonic Cryogenic Tunnel

Characterization of Cavity Flow Fields Using Pressure Data Obtained in the Langley 0.3-Meter Transonic Cryogenic Tunnel
Title Characterization of Cavity Flow Fields Using Pressure Data Obtained in the Langley 0.3-Meter Transonic Cryogenic Tunnel PDF eBook
Author Maureen B. Tracy
Publisher
Pages 40
Release 1993
Genre Aerodynamics, Transonic
ISBN

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Experimental Cavity Pressure Measurements at Subsonic and Transonic Speeds. Static-Pressure Results

Experimental Cavity Pressure Measurements at Subsonic and Transonic Speeds. Static-Pressure Results
Title Experimental Cavity Pressure Measurements at Subsonic and Transonic Speeds. Static-Pressure Results PDF eBook
Author National Aeronautics and Space Adm Nasa
Publisher
Pages 80
Release 2018-11-06
Genre
ISBN 9781730884757

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An experimental investigation was conducted to determine cavity flow-characteristics at subsonic and transonic speeds. A rectangular box cavity was tested in the Langley 8-Foot Transonic Pressure Tunnel at Mach numbers from 0.20 to 0.95 at a unit Reynolds number of approximately 3 x 10(exp 6) per foot. The boundary layer approaching the cavity was turbulent. Cavities were tested over a range of length-to-depth ratios (l/h) of 1 to 17.5 for cavity width-to-depth ratios of 1, 4, 8, and 16. Fluctuating- and static-pressure data in the cavity were obtained; however, only static-pressure data is analyzed. The boundaries between the flow regimes based on cavity length-to-depth ratio were determined. The change to transitional flow from open flow occurs at l/h at approximately 6-8 however, the change from transitional- to closed-cavity flow occurred over a wide range of l/h and was dependent on Mach number and cavity configuration. The change from closed to open flow as found to occur gradually. The effect of changing cavity dimensions showed that if the vlaue of l/h was kept fixed but the cavity width was decreased or cavity height was increased, the cavity pressure distribution tended more toward a more closed flow distribution. Plentovich, E. B. and Stallings, Robert L., Jr. and Tracy, M. B. Langley Research Center...

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports
Title Scientific and Technical Aerospace Reports PDF eBook
Author
Publisher
Pages 602
Release 1995
Genre Aeronautics
ISBN

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Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

Cavity Aeroacoustics

Cavity Aeroacoustics
Title Cavity Aeroacoustics PDF eBook
Author Richard E. Dix
Publisher
Pages 40
Release 1990
Genre Aeroacoustics
ISBN

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NASA Langley Scientific and Technical Information Output: 1997

NASA Langley Scientific and Technical Information Output: 1997
Title NASA Langley Scientific and Technical Information Output: 1997 PDF eBook
Author
Publisher
Pages 162
Release 1998
Genre
ISBN

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High Performance Computing in Science and Engineering, Garching/Munich 2007

High Performance Computing in Science and Engineering, Garching/Munich 2007
Title High Performance Computing in Science and Engineering, Garching/Munich 2007 PDF eBook
Author Siegfried Wagner
Publisher Springer Science & Business Media
Pages 700
Release 2008-10-22
Genre Mathematics
ISBN 3540691820

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For the fourth time, the Leibniz Supercomputing Centre (LRZ) and the Com- tence Network for Technical, Scienti c High Performance Computing in Bavaria (KONWIHR) publishes the results from scienti c projects conducted on the c- puter systems HLRB I and II (High Performance Computer in Bavaria). This book reports the research carried out on the HLRB systems within the last three years and compiles the proceedings of the Third Joint HLRB and KONWIHR Result and Reviewing Workshop (3rd and 4th December 2007) in Garching. In 2000, HLRB I was the rst system in Europe that was capable of performing more than one Tera op/s or one billion oating point operations per second. In 2006 it was replaced by HLRB II. After a substantial upgrade it now achieves a peak performance of more than 62 Tera op/s. To install and operate this powerful system, LRZ had to move to its new facilities in Garching. However, the situation regarding the need for more computation cycles has not changed much since 2000. The demand for higher performance is still present, a trend that is likely to continue for the foreseeable future. Other resources like memory and disk space are currently in suf cient abundance on this new system.