A Tabulation of Wind-tunnel Pressure Data at Mach Numbers of 1.61 and 2.01 of Five Swept Wings of the Same Plan Form But Different Surface Shapes
Author: Frederick Cyril Grant
Publisher:
Published: 1958
Total Pages: 196
ISBN-13:
DOWNLOAD EBOOKRead and Download eBook Full
Author: Frederick Cyril Grant
Publisher:
Published: 1958
Total Pages: 196
ISBN-13:
DOWNLOAD EBOOKAuthor: Jewel B. Barlow
Publisher: John Wiley & Sons
Published: 1999-02-22
Total Pages: 738
ISBN-13: 0471557749
DOWNLOAD EBOOKA 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.
Author: Thomas R. Yechout
Publisher: AIAA
Published: 2003
Total Pages: 666
ISBN-13: 9781600860782
DOWNLOAD EBOOKBased 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.
Author: Robert C. Nelson
Publisher:
Published: 1998
Total Pages: 464
ISBN-13:
DOWNLOAD EBOOKThis edition of this this flight stability and controls guide features an unintimidating math level, full coverage of terminology, and expanded discussions of classical to modern control theory and autopilot designs. Extensive examples, problems, and historical notes, make this concise book a vital addition to the engineer's library.
Author: John David Anderson
Publisher: AIAA
Published: 1989
Total Pages: 710
ISBN-13: 9781563474590
DOWNLOAD EBOOKThis book is a self-contained text for those students and readers interested in learning hypersonic flow and high-temperature gas dynamics. It assumes no prior familiarity with either subject on the part of the reader. If you have never studied hypersonic and/or high-temperature gas dynamics before, and if you have never worked extensively in the area, then this book is for you. On the other hand, if you have worked and/or are working in these areas, and you want a cohesive presentation of the fundamentals, a development of important theory and techniques, a discussion of the salient results with emphasis on the physical aspects, and a presentation of modern thinking in these areas, then this book is also for you. In other words, this book is designed for two roles: 1) as an effective classroom text that can be used with ease by the instructor, and understood with ease by the student; and 2) as a viable, professional working tool for engineers, scientists, and managers who have any contact in their jobs with hypersonic and/or high-temperature flow.
Author: Harvey H. Hubbard
Publisher:
Published: 1991
Total Pages: 620
ISBN-13:
DOWNLOAD EBOOKAuthor: W. Z. Stepniewski
Publisher: Courier Corporation
Published: 2013-04-22
Total Pages: 640
ISBN-13: 0486318516
DOWNLOAD EBOOKDIVClear, concise text covers aerodynamic phenomena of the rotor and offers guidelines for helicopter performance evaluation. Originally prepared for NASA. Prefaces. New Indexes. 10 black-and-white photos. 537 figures. /div
Author: Michael S. Selig
Publisher:
Published: 1989
Total Pages: 424
ISBN-13:
DOWNLOAD EBOOKAuthor: Joseph R. Chambers
Publisher: NASA
Published: 2014
Total Pages: 533
ISBN-13: 9781626830165
DOWNLOAD EBOOKAuthor: Bruce Larrimer
Publisher:
Published: 2020-06-15
Total Pages:
ISBN-13: 9781626830592
DOWNLOAD EBOOK