Download or read book Wind tunnel Tests of a 0 16 scale Model of the X 3 Airplane at High Subsonic Speeds Additional Stability and Control Characteristics and the Aerodynamic Effects of External Stores and Ram Jets written by Joseph W. Cleary and published by . This book was released on 1950 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Index of NACA Technical Publications written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1959 with total page 388 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book A Selected Listing of NASA Scientific and Technical Reports for written by and published by . This book was released on 1957 with total page 388 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind tunnel Tests of a 0 16 scale Model of the X 3 Airplane at High Subsonic Speeds written by William T. Hamilton and published by . This book was released on 1950 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1975 with total page 970 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.
Download or read book Wind tunnel Tests of a 1 12 scale Model of the X 3 Airplane at Subsonic and Supersonic Speeds written by Robert N. Olson and published by . This book was released on 1951 with total page 111 pages. Available in PDF, EPUB and Kindle. Book excerpt: The static longitudinal-, lateral-, and directional-stability and control characteristics of a 1/12-scale model of the Douglas X-3 airplane at subsonic and supersonic Mach numbers are presented. The model was equipped with an all-movable horizontal tail, an aileron on the left wing, and a rudder on the vertical-tail surface. The investigation covered a range of Mach numbers from 0.60 to 0.93 and 1.30 to 1.91 at Reynolds numbers of 980,000 to 2,610,000.
Download or read book Wind tunnel Tests of a 0 16 scale Model of the X 3 Airplane at High Subsonic Speeds written by Joseph W. Cleary and published by . This book was released on 1950 with total page 61 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Large scale Wind tunnel Tests of an Airplane Model with an Unswept Tilt Wing of Aspect Ration 5 5 and with Four Propellers and Blowing Flaps written by James A. Weiberg and published by . This book was released on 1961 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Propfan Test Assessment Testbed Aircraft Stability and Control performance 1 9 scale Wind Tunnel Tests written by and published by . This book was released on 1988 with total page 162 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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:
Download or read book Subsonic Flight Tests of a 1 7 scale Radio controlled Model of the North American X 15 Airplane with Particular Reference to High Angle of attack Conditions written by Donald E. Hewes and published by . This book was released on 1960 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Large scale Wind tunnel Tests at Low Speed of a Delta Winged Supersonic Transport Model in the Presence of the Ground written by and published by . This book was released on 1962 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Introduction to Aircraft Flight Mechanics written by Thomas R. Yechout and published by AIAA. This book was released on 2003 with total page 666 pages. Available in PDF, EPUB and Kindle. Book excerpt: Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.
Download or read book Longitudinal Airplane Dynamics Wind Tunnel Test Equipment written by O. B. Tufts and published by . This book was released on 1955 with total page 246 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aeroacoustics of Flight Vehicles written by Harvey H. Hubbard and published by . This book was released on 1991 with total page 620 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind Tunnel Tests of Fuselages and Windscreens written by Edward Pearson Warner and published by . This book was released on 1925 with total page 552 pages. Available in PDF, EPUB and Kindle. Book excerpt: The tests described herein were made in 1918, in the old four-foot wind tunnel at the Massachusetts Institute of Technology and at the request of the Engineering Division of the U.S. Army Air Service.
Download or read book Low Speed Wind Tunnel Testing written by Jewel B. Barlow and published by John Wiley & Sons. This book was released on 1999-02-22 with total page 738 pages. Available in PDF, EPUB and Kindle. Book excerpt: A brand-new edition of the classic guide on low-speed wind tunnel testing While great advances in theoretical and computational methods have been made in recent years, low-speed wind tunnel testing remains essential for obtaining the full range of data needed to guide detailed design decisions for many practical engineering problems. This long-awaited Third Edition of William H. Rae, Jr.'s landmark reference brings together essential information on all aspects of low-speed wind tunnel design, analysis, testing, and instrumentation in one easy-to-use resource. Written by authors who are among the most respected wind tunnel engineers in the world, this edition has been updated to address current topics and applications, and includes coverage of digital electronics, new instrumentation, video and photographic methods, pressure-sensitive paint, and liquid crystal-based measurement methods. The book is organized for quick access to topics of interest, and examines basic test techniques and objectives of modeling and testing aircraft designs in low-speed wind tunnels, as well as applications to fluid motion analysis, automobiles, marine vessels, buildings, bridges, and other structures subject to wind loading. Supplemented with real-world examples throughout, Low-Speed Wind Tunnel Testing, Third Edition is an indispensable resource for aerospace engineering students and professionals, engineers and researchers in the automotive industries, wind tunnel designers, architects, and others who need to get the most from low-speed wind tunnel technology and experiments in their work.
