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Author : Richard M. Bishop
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book New AEDC Wind Tunnel Capabilities written by Richard M. Bishop and published by . This book was released on 2000 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : T. D. Buchanan
Publisher :
ISBN 13 :
Total Pages : 48 pages
Book Rating : 4.:/5 (227 download)
Download or read book Captive Trajectory System Test Planning Information for AEDC Supersonic Wind Tunnel (A) and Hypersonic Wind Tunnels (B) and (C). written by T. D. Buchanan and published by . This book was released on 1983 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt: Normally in the development of flight vehicle systems, the staging characteristics have to be obtained experimentally. This report briefly describes the specialized methods used in wind tunnel tests at the Arnold Engineering Development Center in simulating the staging process. The capabilities of the mechanisms and the precision to which the data can be obtained are presented, along with descriptions of typical tests. (Author).
Author :
Publisher :
ISBN 13 :
Total Pages : 13 pages
Book Rating : 4.:/5 (946 download)
Download or read book Expected Productivity Benefits Resulting from the New Data Acquisition, Processing, and Control System for Tunnel 16T at AEDC written by and published by . This book was released on 1998 with total page 13 pages. Available in PDF, EPUB and Kindle. Book excerpt: Requirements for large scale transonic wind tunnel test capability into the next century necessitate that significant sustainment efforts be undertaken for U.S. facilities to maintain reliable and efficient testing services. Many national facilities located at the major NASA centers and the Department of Defense's Arnold Engineering Development Center (AEDC) are in the middle of or preparing for major refurbishment programs. In Fiscal Year 1998, the Propulsion Wind Tunnel (PWT) Facility at AEDC launched a 7 year, $80M sustainment program which will improve reliability, reduce testing cycle time, reduce the number of operational station keepers, and improve the quality of test data in the 16 foot transonic and supersonic wind tunnels. A major part of this program is a total replacement of the data acquisition, processing and control systems in Tunnel 16T. This effort will provide major improvements in productivity of the test process as well as improved reliability and quality of data. This effort, along with ongoing maintenance and improvement projects, will sustain the world class status of this important development wind tunnel.
Author : T. D. Buchanan
Publisher :
ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (134 download)
Download or read book Captive Trajectory System for AEDC Supersonic Wind Tunnel (A) and Hypersonic Wind Tunnels (B) and (C) written by T. D. Buchanan and published by . This book was released on 1983 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : W. T. Strike (Jr.)
Publisher :
ISBN 13 :
Total Pages : 120 pages
Book Rating : 4.3/5 (91 download)
Download or read book Calibration and Performance of the AEDC/VKF Tunnel C, Mach Number 4, Aerothermal Wind Tunnel written by W. T. Strike (Jr.) and published by . This book was released on 1982 with total page 120 pages. Available in PDF, EPUB and Kindle. Book excerpt: The shakedown and calibrated characteristics of the new AEDC Mach Number 4 Aerothermal Wind Tunnel were experimentally identified at several test conditions. The nominal Mach number of the test core as defined by a 30-probe pitot pressure rake varied between nominally 3.95 and 4.0, depending on the test section Reynolds number and stilling chamber temperature. The overall variation in the stilling chamber pressure is nominally 15 to 180 psia, with temperatures from 250 to 1,210 F for an overall Reynolds number range of 0.2 to 8.1 million per foot and true temperature-pressure altitude simulation from 56,000 to 105,000 ft. (Author).
Author : Frank K. Lu
Publisher : AIAA
ISBN 13 : 9781600864483
Total Pages : 694 pages
Book Rating : 4.8/5 (644 download)
Download or read book Advanced Hypersonic Test Facilities written by Frank K. Lu and published by AIAA. This book was released on 2002 with total page 694 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Philip S. Antón
Publisher : Minnesota Historical Society
ISBN 13 : 9780833036421
Total Pages : 166 pages
Book Rating : 4.0/5 (364 download)
Download or read book Wind Tunnel and Propulsion Test Facilities written by Philip S. Antón and published by Minnesota Historical Society. This book was released on 2004 with total page 166 pages. Available in PDF, EPUB and Kindle. Book excerpt: The National Aeronautics and Space Administration's (NASA's) wind tunnel and propulsion test facilities continue to be important to U.S. competitiveness across the military, commercial, and space sectors. Unfortunately, management issues are creating real risks to these facilities. This technical report supports a companion monograph (Wind Tunnel and Propulsion Test Facilities: An Assessment of NASA's Capabilities to Serve National Needs, MG-178-NASA/OSD), providing more detailed data, observations, and conclusions about the future of NASA's wind tunnel and propulsion test facilities.
Author : R. L. Palko
Publisher :
ISBN 13 :
Total Pages : 136 pages
Book Rating : 4.:/5 (227 download)
Download or read book A Method to Increase the Full-Scale Inlet/Engine System Testing Capability of the AEDC 16-ft Transonic Wind Tunnel written by R. L. Palko and published by . This book was released on 1973 with total page 136 pages. Available in PDF, EPUB and Kindle. Book excerpt: A study was conducted of a new testing technique using flow shaping that together with some modifications of the AEDC 16-ft Transonic Propulsion Wind Tunnel will provide the capability to test full-scale inlet/engine configurations with forebody effects at high maneuvering angles at transonic velocities. The method used to obtain the flow simulation for high maneuvering angles utilized auxiliary flow shaping and geometric pitch. An analytical potential flow method was used to determine the configuration of devices necessary to produce the required flow fields; these devices were then checked experimentally to verify the results. (Modified author abstract).
Author : Philip S. Antón
Publisher : Minnesota Historical Society
ISBN 13 : 9780833035905
Total Pages : 144 pages
Book Rating : 4.0/5 (359 download)
Download or read book Wind Tunnel and Propulsion Test Facilities written by Philip S. Antón and published by Minnesota Historical Society. This book was released on 2004 with total page 144 pages. Available in PDF, EPUB and Kindle. Book excerpt: The National Aeronautics and Space Administration's (NASA's) wind tunnel and propulsion test facilities continue to be important to U.S. competitiveness across the military, commercial, and space sectors. Unfortunately, management issues are creating real risks to these facilities. NASA needs to develop an aeronautics test technology vision and plan; analyze the viability of a national test facility plan; identify and maintain its minimum set of facilities; and identify financial shared support to keep its underutilized but essential facilities from entering financial collapse.
Author : B. H. Goethert
Publisher :
ISBN 13 :
Total Pages : 420 pages
Book Rating : 4.X/5 (3 download)
Download or read book Transonic Wind Tunnel Testing written by B. H. Goethert and published by . This book was released on 2007 with total page 420 pages. Available in PDF, EPUB and Kindle. Book excerpt: Numerous aspects of transonic aerodynamics include wall interference corrections in conventional wind tunnels, subsonic flow in a variety of wind tunnels, and test results from transonic wind tunnels. 1961 edition.
Author : David M. Cahill
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book Implementation of New Wind Tunnel Data Reduction Techniques at the AEDC written by David M. Cahill and published by . This book was released on 2001 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 220 pages
Book Rating : 4.F/5 ( download)
Download or read book Engine Airframe Integration written by and published by . This book was released on 1992 with total page 220 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : P. B. Stich
Publisher :
ISBN 13 :
Total Pages : 109 pages
Book Rating : 4.:/5 (227 download)
Download or read book Mathematical Modeling of the AEDC (Arnold Engineering Development Center) Propulsion Wind Tunnel (16T). written by P. B. Stich and published by . This book was released on 1985 with total page 109 pages. Available in PDF, EPUB and Kindle. Book excerpt: An empirically based model of the 16-ft transonic Wind Tunnel (16T) in the Propulsion Wind Tunnel Facility at the Arnold Engineering Development Center, has been developed for calculating the distribution of tunnel component pressure losses and the effect of changes in these pressure losses on the tunnel total-power requirements. The model consists of two separate computer programs. The Historical Program assesses tunnel performance from a historical data base which was acquired during prior tunnel operation. The Analytical Model uses component pressure-loss information calculated by the Historical Program to evaluate potential changes in tunnel component pressure losses with respect to the tunnel power. The model was used to asess the potential power savings for a modification to the Tunnel 16T diffuser which involves the replacment of the compressor protective screen. Results indicate that for each 1-percent increase in diffuser recovery, a 4-percent decrease in main drive power will result. Less significant power savings were found for improvements to the other tunnel components. Additional keywords: Flow equations, Thermodynamics, Computations. (Author).
Author :
Publisher :
ISBN 13 :
Total Pages : 34 pages
Book Rating : 4.:/5 (317 download)
Download or read book Flight and Wind-tunnel Correlation of Boundary-layer Transition on the AEDC Transition Cone written by and published by . This book was released on 1982 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : J. P. Christopher
Publisher :
ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (227 download)
Download or read book Captive-trajectory Store-separation System of the Aedc-pwt 4-foot Transonic Tunnel written by J. P. Christopher and published by . This book was released on 1968 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: The captive-trajectory store-separation system of the Aerodynamic Wind Tunnel, Transonic (4T), provides the capability for determining the separation trajectory of a store in the vicinity of the parent aircraft. This system may also be used as a six-degree-of-freedom support for conventional force tests with or without a parent installed, and as a pressure probe or transducer mounting platform for flow field surveys in the vicinity of a model. With the store and parent independently supported in the tunnel, trajectory generation involves measurement of forces and moments acting on the captive store model, converting these to full-scale adding other forces and moments which may be applied to the full-scale store, solving the equations of motion for store acceleration, integrating these equations to find store displacement, converting this movement to model scale, and physically moving the store model along its flight path. This report describes the captive-trajectory store-separation system and its testing capabilities and presents the technique used for trajectory generation. (Author).
Author : Thomas Loeser
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book Development of the Dynamic Wind Tunnel Testing Capabilities at DNW-NWB written by Thomas Loeser and published by . This book was released on 2003 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 26 pages
Book Rating : 4.:/5 (317 download)
Download or read book Cryogenic Wind Tunnels: Unique Capabilities for the Aerodynamicist written by and published by . This book was released on 1976 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
