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Comparison Of Wind Tunnel And Flight Measured Base Pressures From The Sharp Leading Edge Upper Vertical Fin Of The X 15 Airplane For Turbulent Flow At Mach Numbers From 1 5 To 5 0 Book in PDF, ePub and Kindle version is available to download in english. Read online anytime anywhere directly from your device. Click on the download button below to get a free pdf file of Comparison Of Wind Tunnel And Flight Measured Base Pressures From The Sharp Leading Edge Upper Vertical Fin Of The X 15 Airplane For Turbulent Flow At Mach Numbers From 1 5 To 5 0 book. This book definitely worth reading, it is an incredibly well-written.
Author : Sheryll Goecke Powers
Publisher : Unknown
Page : 44 pages
File Size : 54,7 Mb
Release : 1971
Category : Drag (Aerodynamics)
ISBN : UIUC:30112106747535
Author : Anonim
Publisher : Unknown
Page : 686 pages
File Size : 40,9 Mb
Release : 1973
Category : Electronic
ISBN : MINN:31951000846449T
Author : Anonim
Publisher : Unknown
Page : 128 pages
File Size : 45,6 Mb
Release : 1972
Category : Aeronautics
ISBN : UIUC:30112075687779
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA).
Author : Anonim
Publisher : Unknown
Page : 942 pages
File Size : 49,7 Mb
Release : 1971
Category : Engineering
ISBN : MSU:31293017237128
Author : Anonim
Publisher : Unknown
Page : 1908 pages
File Size : 53,7 Mb
Release : 1971
Category : Technology
ISBN : COLUMBIA:CU10087621
Author : Anonim
Publisher : Unknown
Page : 1346 pages
File Size : 52,7 Mb
Release : 1985
Category : Aeronautics
ISBN : UIUC:30112075701224
Author : Wendell H. Stillwell
Publisher : Unknown
Page : 140 pages
File Size : 41,5 Mb
Release : 1965
Category : X-15 (Rocket aircraft).
ISBN : UIUC:30112000417359
Author : Jewel B. Barlow,William H. Rae,Alan Pope
Publisher : John Wiley & Sons
Page : 738 pages
File Size : 47,8 Mb
Release : 1999-02-22
Category : Technology & Engineering
ISBN : 9780471557746
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.
Author : Robert C. Nelson
Publisher : WCB/McGraw-Hill
Page : 441 pages
File Size : 52,9 Mb
Release : 1998
Category : Aerodynamique / Aeronautique / Aerospatial / Automatique / Avion / Commande / Conception / Controle / Navigation / Stabilite
ISBN : 0071158383
The second edition of Flight Stability and Automatic Control presents an organized introduction to the useful and relevant topics necessary for a flight stability and controls course. Not only is this text presented at the appropriate mathematical level, it also features standard terminology and nomenclature, along with expanded coverage of classical control theory, autopilot designs, and modern control theory. Through the use of extensive examples, problems, and historical notes, author Robert Nelson develops a concise and vital text for aircraft flight stability and control or flight dynamics courses.
Author : Donald L. Loving
Publisher : Unknown
Page : 20 pages
File Size : 43,9 Mb
Release : 1966
Category : Aerodynamic load
ISBN : UIUC:30112106686881
Author : Harvey H. Hubbard
Publisher : Unknown
Page : 620 pages
File Size : 44,9 Mb
Release : 1991
Category : Aerodynamic noise
ISBN : STANFORD:36105024722329
Author : Franz Wilhelm Schmitz
Publisher : Unknown
Page : 218 pages
File Size : 44,5 Mb
Release : 1967
Category : Aerodynamics
ISBN : PSU:000022807830
Author : A. Elsenaar,Travis W. Binion,E. Stanewsky
Publisher : Unknown
Page : 82 pages
File Size : 53,6 Mb
Release : 1988
Category : Aerodynamics, Transonic
ISBN : 9283504925
Reynolds number effects in transonic flow are critically reviewed. This review, which may be considered a supplement to AR 224 'Boundary Layer Simulation and Control in Wind Tunnels', is mainly concered with a discussion of viscous effects actually observed on realistic configurations. The following geometries are considered: Airfoils and high aspect ratio wings typical and transport aircraft, fighter-type low aspect ratio delta wings, tow- and three-dimensional bodies characteristic of missiles and combat aircraft fuselages, and afterbodies. "Pseudo"--Reynolds number on the wind tunnel environment and in turn affect the flow about a model. As an introduction, a brief retrospect of the "history" of Reynolds number effect is presented. This AGARDograph has been produced at the request of the Fluid Dynamics Panel of AGARD.
Author : Jack Norman Nielsen
Publisher : AIAA (American Institute of Aeronautics & Astronautics)
Page : 450 pages
File Size : 40,8 Mb
Release : 1988-01-01
Category : Guided missiles
ISBN : 0962062901
The similarities between the airplane and the missile extend beyond their flying capabilities, and at higher operational speeds, the configuration distinctions become even less apparent. " Missile Aerodynamics," a classic now available from AIAA and Nielsen Engineering and Research, Inc., combines the best of missile and airplane aerodynamics, drawing extensively from numerous technical papers to present a rational and unified account of the principles behind missile projection. Evaluate the missile versus the airplane in a multitude of areas, from longitudinal acceleration, wing loading, roll and dynamic stability, guidance and navigation, and more. J.N. Nielsen covers every aspect of missile aerodynamics, from the classification of missiles and basic formulas to innovative aerodynamic controls. In one reliable reference, readers will find hundreds of schematics, equations, and tables with practical applications in missile design and engineering. Originally published by Nielsen Engineering and Research, Inc.
Author : Anonim
Publisher : AIAA
Page : 542 pages
File Size : 55,7 Mb
Release : 1990
Category : Boundary layer
ISBN : 1600863787