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A Wind Tunnel Investigation Of Three Nasa 1 Series Inlets At Mach Numbers Up To 092
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Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722915704 Total Pages :184 pages Book Rating :4.9/5 (157 download)
Book Synopsis A Wind Tunnel Investigation of Three NACA 1-Series Inlets at Mach Numbers Up To 0. 92 by : National Aeronautics and Space Administration (NASA)
Download or read book A Wind Tunnel Investigation of Three NACA 1-Series Inlets at Mach Numbers Up To 0. 92 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 184 pages. Available in PDF, EPUB and Kindle. Book excerpt: Pressure distributions on three NACA 1-series inlets have been obtained in the Langley 16-Foot Transonic Tunnel. The cowl diameter ratio (ratio of cowl highlight diameter to cowl maximum diameter) was 0.85 for all three inlets. The cowl length ratio (ratio of cowl length to cowl maximum diameter) was 1.0 for two of the inlets (NACA 1-85-100) and 0.439 for the other (NACA 1-85-43.9) inlet. One of the inlets with a cowl length ratio of 1.0 had an internal contraction ratio (ratio of highlight area to throat area) of 1.009 and the other had a contraction ratio of 1.250. The inlet with a cowl length ratio of 0.439 also had an internal contraction ratio of 1.250. All three inlets had longitudinal rows of static pressure orifices on the top and bottom external cowl surfaces. The inlet with a contraction ratio of 1.009 also had a row of static pressure orifices on the side of the cowl (external surface). The two inlets with a contraction ratio of 1.250 had a longitudinal row of static pressure orifices on the diffuser surface. Re, Richard J. and Abeyounis, William K. Langley Research Center WIND TUNNEL TESTS; PRESSURE DISTRIBUTION; STATIC PRESSURE; ENGINE INLETS; AIRCRAFT ENGINES; MACH NUMBER; ANGLE OF ATTACK; SUBSONIC FLOW; CONTRACTION; NACELLES; FOREBODIES; MASS FLOW; PRESSURE MEASUREMENT; AXISYMMETRIC BODIES...
Book Synopsis A Wind Tunnel Investigation of Three NASA 1-series Inlets at Mach Numbers Up to 0.92 by : Richard J. Re
Download or read book A Wind Tunnel Investigation of Three NASA 1-series Inlets at Mach Numbers Up to 0.92 written by Richard J. Re and published by . This book was released on 1996 with total page 180 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Wind Tunnel Investigation of Three NACA 1-Series Inlets at Mach Numbers Up to 0.92 by :
Download or read book A Wind Tunnel Investigation of Three NACA 1-Series Inlets at Mach Numbers Up to 0.92 written by and published by . This book was released on 1996 with total page 188 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Wind Tunnel Investigation of Three NACA 1-series Inlets at Mach Numbers Up to 0.92 by : Richard J. Re
Download or read book A Wind Tunnel Investigation of Three NACA 1-series Inlets at Mach Numbers Up to 0.92 written by Richard J. Re and published by . This book was released on 1996 with total page 180 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Memorandum written by and published by . This book was released on 1994 with total page 492 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An investigation of several NACA 1-series inlets at Mach numbers from 0.4 to 1.29 for mass-flow ratios near 1.0 by : Richard J. Re
Download or read book An investigation of several NACA 1-series inlets at Mach numbers from 0.4 to 1.29 for mass-flow ratios near 1.0 written by Richard J. Re and published by . This book was released on 1976 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind Tunnel Investigation of Three Axisymmetric Cowls of Different Lengths at Mach Numbers from 0.60 to 0.92 by : Richard J. Re
Download or read book Wind Tunnel Investigation of Three Axisymmetric Cowls of Different Lengths at Mach Numbers from 0.60 to 0.92 written by Richard J. Re and published by . This book was released on 1993 with total page 292 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind Tunnel Investigation of Three Axisymmetric Cowls of Different Lenghts at Mach Numbers from 0.60 to 0.92 by : Richard J. Re
Download or read book Wind Tunnel Investigation of Three Axisymmetric Cowls of Different Lenghts at Mach Numbers from 0.60 to 0.92 written by Richard J. Re and published by . This book was released on 1993 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Monthly Catalog, United States Public Documents by : United States. Superintendent of Documents
Download or read book Monthly Catalog, United States Public Documents written by United States. Superintendent of Documents and published by . This book was released on 1973 with total page 1252 pages. Available in PDF, EPUB and Kindle. Book excerpt: February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index.
Book Synopsis Wind Tunnels of NASA by : Donald D. Baals
Download or read book Wind Tunnels of NASA written by Donald D. Baals and published by . This book was released on 1981 with total page 218 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 542 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis NASA Langley Scientific and Technical Information Output: 1996 by :
Download or read book NASA Langley Scientific and Technical Information Output: 1996 written by and published by . This book was released on 1997 with total page 180 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of a Mixed Compression Axisymmetric Inlet at Mach Number 5.3 by : Eldon A. Latham
Download or read book Investigation of a Mixed Compression Axisymmetric Inlet at Mach Number 5.3 written by Eldon A. Latham and published by . This book was released on 1972 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind Tunnel Tests of Two-dimensional and Half-axisymmetric Inlet Models at Mach Numbers 1.5 Through 3.0 by : Frederick K. Hube
Download or read book Wind Tunnel Tests of Two-dimensional and Half-axisymmetric Inlet Models at Mach Numbers 1.5 Through 3.0 written by Frederick K. Hube and published by . This book was released on 1970 with total page 278 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Government Reports Announcements & Index by :
Download or read book Government Reports Announcements & Index written by and published by . This book was released on 1993 with total page 602 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722402617 Total Pages :78 pages Book Rating :4.4/5 (26 download)
Book Synopsis Flowfield Measurements in the NASA Lewis Research Center 9- By 15-Foot Low-Speed Wind Tunnel by : National Aeronautics and Space Administration (NASA)
Download or read book Flowfield Measurements in the NASA Lewis Research Center 9- By 15-Foot Low-Speed Wind Tunnel written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-06 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation was conducted in the NASA Lewis 9- by 15-Foot Low-Speed Wind Tunnel to determine the flow characteristics in the test section during wind tunnel operation. In the investigation, a 20-probe horizontally-mounted Pitot-static flow survey rake was used to obtain cross-sectional total and static pressure surveys at four axial locations in the test section. At each axial location, the cross-sectional flowfield surveys were made by repositioning the Pitot-static flow survey rake vertically. In addition, a calibration of the new wind tunnel rake instrumentation, used to determine the wind tunnel operating conditions, was performed. Boundary laser surveys were made at three axial locations in the test section. The investigation was conducted at tunnel Mach numbers 0.20, 0.15, 0.10, and 0.05. The test section profile results from the investigation indicate that fairly uniform total pressure profiles (outside the test section boundary layer) and fairly uniform static pressure and Mach number profiles (away from the test section walls and downstream of the test section entrance) exist throughout in the wind tunnel test section. Hughes, Christopher E. Glenn Research Center...
Book Synopsis Wind Tunnel Investigation of Three Proposed Launch Vehicles at Mach Numbers from 2.30 to 4.63 by : A. B. Blair
Download or read book Wind Tunnel Investigation of Three Proposed Launch Vehicles at Mach Numbers from 2.30 to 4.63 written by A. B. Blair and published by . This book was released on 1968 with total page 65 pages. Available in PDF, EPUB and Kindle. Book excerpt:
