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Scale Model Studies Of The Proposed V Stol Test Facility Inside The Existing 7 X 10 Foot Transonic Wind Tunnel
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Book Synopsis Scale-model Studies of the Proposed V/STOL Test Facility Inside the Existing 7 X 10 Foot Transonic Wind Tunnel by : P. S. Barna
Download or read book Scale-model Studies of the Proposed V/STOL Test Facility Inside the Existing 7 X 10 Foot Transonic Wind Tunnel written by P. S. Barna and published by . This book was released on 1980 with total page 106 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Full Scale Subsonic Wind Tunnel Requirements and Design Studies by : Mark W. Kelly
Download or read book Full Scale Subsonic Wind Tunnel Requirements and Design Studies written by Mark W. Kelly and published by . This book was released on 1972 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scale Model Studies on the Proposed V/STOL Test Facility by : P. S. Barna
Download or read book Scale Model Studies on the Proposed V/STOL Test Facility written by P. S. Barna and published by . This book was released on 1981 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Large-scale V/STOL Testing written by and published by . This book was released on 1977 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind Tunnel Model Parametric Study for Use in the Proposed 8 Ft X 10 Ft High Reynolds Number Transonic Wind Tunnel (HIRT) at Arnold Engineering Development Center by : Walter K. Alexander
Download or read book Wind Tunnel Model Parametric Study for Use in the Proposed 8 Ft X 10 Ft High Reynolds Number Transonic Wind Tunnel (HIRT) at Arnold Engineering Development Center written by Walter K. Alexander and published by . This book was released on 1973 with total page 197 pages. Available in PDF, EPUB and Kindle. Book excerpt: The need for a high Reynolds number transonic wind tunnel (HIRT) has been recognized throughout the industry for some years. The proposed HIRT facility at Arnold Engineering Development Center will provide a much needed tool for the study of phenomena sensitive to Reynolds number. The usefulness of the HIRT facility will be largely influenced by the ability of industry to design and build wind-tunnel models for an acceptable cost capable of operating within the severe environment of the tunnel. The object of this study is to determine the feasibility of designing and building models capable of withstanding the loads and environmental conditions of the facility. The aircraft configurations chosen for study cover a wide spectrum of flight conditions. (Modified author abstract).
Book Synopsis Experimental Study of Wind-tunnel Wall Effects and Wall Corrections for a General-research V/STOL Tilt-wing Model with Flap by : Kalman J. Grunwald
Download or read book Experimental Study of Wind-tunnel Wall Effects and Wall Corrections for a General-research V/STOL Tilt-wing Model with Flap written by Kalman J. Grunwald and published by . This book was released on 1965 with total page 122 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 1984 with total page 688 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Book Synopsis The David Taylor Model Basin 7- by 10-foot Transonic Wind Tunnel Facility by : Walter S. Thomas
Download or read book The David Taylor Model Basin 7- by 10-foot Transonic Wind Tunnel Facility written by Walter S. Thomas and published by . This book was released on 1960 with total page 35 pages. Available in PDF, EPUB and Kindle. Book excerpt: A description is given of the David Taylor Model Basin 7-by 10-ft transonic wind tunnel. Information is given which should aid in preliminary model design. Emphasis is placed on the versatility of 2 model support systems which may be used simultaneously to provide rapid studies of trajectories and various downstream surveys. (Author).
Book Synopsis Wind-tunnel Data from a 0.16-scale V/STOL Model with Direct-lift and Lift-cruise Jets by : Matthew M. Winston
Download or read book Wind-tunnel Data from a 0.16-scale V/STOL Model with Direct-lift and Lift-cruise Jets written by Matthew M. Winston and published by . This book was released on 1969 with total page 84 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 1986 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind Tunnel Test Techniques by : Colin Britcher
Download or read book Wind Tunnel Test Techniques written by Colin Britcher and published by Academic Press. This book was released on 2023-10-20 with total page 672 pages. Available in PDF, EPUB and Kindle. Book excerpt: Wind Tunnel Test Techniques: Design and Use at Low and High Speeds with Statistical Engineering Applications provides an up-to-date treatment of the topic. Beginning with a brief history of wind tunnels and its types and uses, the book goes on to cover subsonic, supersonic and hypersonic wind tunnel design and construction, calibration, boundary corrections, flow quality assessment, pressure surveys, and dynamic testing. It also focuses on wind tunnel facilities, making it useful for both the designer and operator. Engineers and graduate students in aerospace, automotive and similar programs will find this book useful in their work with experimental aerodynamics, gas dynamics, facility design and performance. - Deals with a broad range of flow speeds in wind tunnels, from low speed to high speed - Provides a discussion of similarity laws as well as material on statistical analysis - Includes coverage on facility-to-facility and facility-to-CFD correlation - Presents advanced topics such as cryogenic wind tunnels, ground simulation in automotive testing, and propulsion testing
Book Synopsis Plan for Conversion of DTNSRDC 7- X 10-Foot Transonic Wind Tunnel to Provide V/STOL Capability by : Thomas M. Clancy
Download or read book Plan for Conversion of DTNSRDC 7- X 10-Foot Transonic Wind Tunnel to Provide V/STOL Capability written by Thomas M. Clancy and published by . This book was released on 1975 with total page 19 pages. Available in PDF, EPUB and Kindle. Book excerpt: A plan is presented for adding a 12- x 15-foot V/STOL test section in the return leg of the 7- x 10-foot transonic wind tunnel at the David W. Taylor Naval Ship Research and Development Center (DTNSRDC). Features include (1) an inflatable bellmouth which is collapsible/removable to permit conversion from V/STOL to transonic operation on a quick turnaround basis and (2) provision for opening roof doors in the V/STOL section to permit low-speed operation in an alternate section 22 feet high by 15 feet wide. (Author).
Book Synopsis Wind-tunnel Investigation of V/STOL Transport Model with Six Wing-mounted Lift Fans by : William A. Newsom
Download or read book Wind-tunnel Investigation of V/STOL Transport Model with Six Wing-mounted Lift Fans written by William A. Newsom and published by . This book was released on 1970 with total page 134 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Assessment of Aerodynamic Performance of V/STOL and STOVL Fighter Aircraft by :
Download or read book Assessment of Aerodynamic Performance of V/STOL and STOVL Fighter Aircraft written by and published by . This book was released on 1984 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :GENERAL ELECTRIC CO CINCINNATI OHIO ADVANCED ENGINE AND TECHNOLOGY Dept Publisher : ISBN 13 : Total Pages :547 pages Book Rating :4.:/5 (227 download)
Book Synopsis Wind Tunnel Test Report Conventional Model. Volume Iii. High Speed (mach by : GENERAL ELECTRIC CO CINCINNATI OHIO ADVANCED ENGINE AND TECHNOLOGY Dept
Download or read book Wind Tunnel Test Report Conventional Model. Volume Iii. High Speed (mach written by GENERAL ELECTRIC CO CINCINNATI OHIO ADVANCED ENGINE AND TECHNOLOGY Dept and published by . This book was released on 1964 with total page 547 pages. Available in PDF, EPUB and Kindle. Book excerpt: The volume presents the results of high speed wind tunnel test of a one-eighth scale model of the U.S. Army XV-5A Lift Fan Research Aircraft. The tests were conducted at the David Taylor Model Basin 7 x 10 foot Transonic Wind Tunnel Facility. Conventional model force, pressure, and hinge moment data were obtained over a Mach number range of .40 to .90 and pitch and sideslip ranges of -4 to 15 degrees and -5 to +5 degrees respectively. The complete aircraft was the primary configuration tested, with the majority of the variations being in control surface and stabilizer settings. Tests were also conducted with the vertical and horizontal tail surfaces removed, with wing fan upper and lower surface strut fairings removed, and with engine duct pressure survey rake installed. (Author).
Book Synopsis Wind Tunnel Test Data Report of a Powered 1/5 Scale ARL/Bell V/STOL Aircraft Model. Phase II. by : P. E. Ryan
Download or read book Wind Tunnel Test Data Report of a Powered 1/5 Scale ARL/Bell V/STOL Aircraft Model. Phase II. written by P. E. Ryan and published by . This book was released on 1969 with total page 214 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tests of a 1/5 scale powered V/STOL aircraft model were conducted in the Langley 7 x 10 wind tunnel. Vehicle aerodynamics and stability and control characteristics were investigated. The test results are presented without analysis.
Book Synopsis A Collection of Technical Papers by :
Download or read book A Collection of Technical Papers written by and published by . This book was released on 1978 with total page 786 pages. Available in PDF, EPUB and Kindle. Book excerpt:
