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Nol Hypersonic Tunnel No 4 Results Viii Development And Calibration Of Mass Flow Probes In Hypersonic Flow
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Book Synopsis Nol Hypersonic Tunnel No. 4 Results Viii: Development and Calibration of Mass Flow Probes in Hypersonic Flow by : L. L. LICCINI
Download or read book Nol Hypersonic Tunnel No. 4 Results Viii: Development and Calibration of Mass Flow Probes in Hypersonic Flow written by L. L. LICCINI and published by . This book was released on 1955 with total page 23 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis NOL Hypersonic Tunnel No. 4 by : James E. Danberg
Download or read book NOL Hypersonic Tunnel No. 4 written by James E. Danberg and published by . This book was released on 1964 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt: NOL's Hypersonic Tunnel No. 4 is a continuous blow-down hypersonic tunnel designed for research and development testing of models, instrumentation, and wind tunnel components. It can operate at Mach numbers from 5 to 10 with supply pressures up to 52 atmospheres and supply temperatures up to 1700 R. This report summarizes the pertinent aerodynamic design criteria and operating experience compiled during its first eleven years of operation. Included are descriptions of the major components and their performance along with the flight simulation capability of the facility and a bibliography of previously published reports. (Author).
Download or read book NASA Technical Note written by and published by . This book was released on 1969 with total page 812 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Performance of a Mass-flux Probe in a Mach 3 Stream by : Lloyd N. Krause
Download or read book Performance of a Mass-flux Probe in a Mach 3 Stream written by Lloyd N. Krause and published by . This book was released on 1969 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: Performance of mass flux probe in Mach 3 stream.
Download or read book Title Announcement Bulletin written by and published by . This book was released on 1956 with total page 576 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis U.S. Government Research Reports by :
Download or read book U.S. Government Research Reports written by and published by . This book was released on 1959 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Description and Calibration of the Langley Hypersonic CF4 Tunnel: A Facility for Simulating Low Gamma Flow as Occurs for a Real Gas by :
Download or read book Description and Calibration of the Langley Hypersonic CF4 Tunnel: A Facility for Simulating Low Gamma Flow as Occurs for a Real Gas written by and published by . This book was released on 1985 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis International Aerospace Abstracts by :
Download or read book International Aerospace Abstracts written by and published by . This book was released on 1969 with total page 710 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Total Temperature Probes for High-temperature Hypersonic Boundary-layer Measurements by : Cindy W. Albertson
Download or read book Total Temperature Probes for High-temperature Hypersonic Boundary-layer Measurements written by Cindy W. Albertson and published by . This book was released on 1993 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Corrections to Single-Shielded Total Temperature Probes in Subsonic, Supersonic, and Hypersonic Flow by :
Download or read book Corrections to Single-Shielded Total Temperature Probes in Subsonic, Supersonic, and Hypersonic Flow written by and published by . This book was released on 1976 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: A new total temperature measurement correction is developed for the single-shielded type of probe. This method is based on a detailed analysis of the coupled heat transfer-viscous flow region existing within the probe. The correction is valid for all flow-field conditions and requires probe calibration data only in the free stream where flow properties are known. Total temperature measurements on the windward ray of a 4-deg sharp cone at Mach 10 in AEDC Hypersonic Tunnel (C) are used in conjunction with corresponding theoretical predictions to substantiate the present analysis. The new approach appears to be a significant improvement over present methods. (Author).
Book Synopsis Computational Method to Predict Thermodynamic, Transport, and Flow Properties for the Modified Langley 8-foot High-temperature Tunnel by : S. Venkateswaran
Download or read book Computational Method to Predict Thermodynamic, Transport, and Flow Properties for the Modified Langley 8-foot High-temperature Tunnel written by S. Venkateswaran and published by . This book was released on 1992 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Description and Initial Calibration of the Langley 12-inch Hypersonic Ceramic-heated Tunnel by : Louis E. Clark
Download or read book Description and Initial Calibration of the Langley 12-inch Hypersonic Ceramic-heated Tunnel written by Louis E. Clark and published by . This book was released on 1965 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Description and Initial Calibration of the Langley 20-inch Hypersonic Arc-heated Tunnel by : Raymond E. Midden
Download or read book Description and Initial Calibration of the Langley 20-inch Hypersonic Arc-heated Tunnel written by Raymond E. Midden and published by . This book was released on 1968 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Bibliography of Scientific and Industrial Reports by :
Download or read book Bibliography of Scientific and Industrial Reports written by and published by . This book was released on 1959 with total page 874 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation of the Aerodynamic Pressures on the Apollo Launch Escape Vehicle Configuration by : William C. Moseley (Jr.)
Download or read book Wind-tunnel Investigation of the Aerodynamic Pressures on the Apollo Launch Escape Vehicle Configuration written by William C. Moseley (Jr.) and published by . This book was released on 1970 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Development of a High Accuracy Angular Measurement System for Langley Research Center Hypersonic Wind Tunnel Facilities by :
Download or read book Development of a High Accuracy Angular Measurement System for Langley Research Center Hypersonic Wind Tunnel Facilities written by and published by . This book was released on 2003 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781721132218 Total Pages :114 pages Book Rating :4.1/5 (322 download)
Book Synopsis Development of a High Accuracy Angular Measurement System for Langley Research Center Hypersonic Wind Tunnel Facilities by : National Aeronautics and Space Administration (NASA)
Download or read book Development of a High Accuracy Angular Measurement System for Langley Research Center Hypersonic Wind Tunnel Facilities written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-06-15 with total page 114 pages. Available in PDF, EPUB and Kindle. Book excerpt: Modern experimental and test activities demand innovative and adaptable procedures to maximize data content and quality while working within severely constrained budgetary and facility resource environments. This report describes development of a high accuracy angular measurement capability for NASA Langley Research Center hypersonic wind tunnel facilities to overcome these deficiencies. Specifically, utilization of micro-electro-mechanical sensors including accelerometers and gyros, coupled with software driven data acquisition hardware, integrated within a prototype measurement system, is considered. Development methodology addresses basic design requirements formulated from wind tunnel facility constraints and current operating procedures, as well as engineering and scientific test objectives. Description of the analytical framework governing relationships between time dependent multi-axis acceleration and angular rate sensor data and the desired three dimensional Eulerian angular state of the test model is given. Calibration procedures for identifying and estimating critical parameters in the sensor hardware is also addressed. Newman, Brett and Yu, Si-bok and Rhew, Ray D. (Technical Monitor) Langley Research Center RTOP 718-20-01-01
