Development Of Flow Distortions In A Full Scale Nacelle Inlet At Mach Numbers 0 63 And 1 6 To 2 0
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Development Of Flow Distortions In A Full Scale Nacelle Inlet At Mach Numbers 0 63 And 1 6 To 2 0
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Author : Thomas G. Piercy
language : en
Publisher:
Release Date : 1956
Development Of Flow Distortions In A Full Scale Nacelle Inlet At Mach Numbers 0 63 And 1 6 To 2 0 written by Thomas G. Piercy and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1956 with Aerodynamics, Supersonic categories.
International Aerospace Abstracts
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Author :
language : en
Publisher:
Release Date : 1998
International Aerospace Abstracts written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1998 with Aeronautics categories.
Documentation Of The Phase Iii 0 192 Scale Northrop Mcdonnell Douglas F 18 Inlet Performance Test At Mach Numbers 0 To 1 55
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Author : Jimmy Walker
language : en
Publisher:
Release Date : 1978
Documentation Of The Phase Iii 0 192 Scale Northrop Mcdonnell Douglas F 18 Inlet Performance Test At Mach Numbers 0 To 1 55 written by Jimmy Walker and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1978 with Jet engines categories.
Results Of A 0 2 Scale B 1 Inlet Verification Model Test At Transonic And Supersonic Mach Numbers
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Author : John F. Riddell
language : en
Publisher:
Release Date : 1972
Results Of A 0 2 Scale B 1 Inlet Verification Model Test At Transonic And Supersonic Mach Numbers written by John F. Riddell and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1972 with Airplanes categories.
Results are presented of a wind tunnel investigation of a 0.2-scale model of the left-hand dual-inlet air induction system of the B-1 aircraft. The test was conducted at Mach numbers from 0.55 to 2.3 over an angle-of-attack range from -2 to 13 deg and yaw angles of -6 to 6 deg. Inlet performance in terms of compressor-face total-pressure recovery, total-pressure distortion and turbulence index is presented as a function of engine-face mass-flow ratio for various inlet geometries and model attitudes. Generally, increasing angle of attack caused greated decreases in the performance of the inboard inlet at supersonic Mach numbers and of the outboard inlet at subsonic Mach numbers. Noticeable effects occurred when the structural mode control vanes were varied at the subsonic Mach number at low angles of attack and at negative yaw. (Author).
Aeroacoustics Of Flight Vehicles
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Author : Harvey H. Hubbard
language : en
Publisher:
Release Date : 1991
Aeroacoustics Of Flight Vehicles written by Harvey H. Hubbard and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1991 with Aerodynamic noise categories.
Advanced Turboprop Project
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Author : Roy D. Hager
language : en
Publisher:
Release Date : 1988
Advanced Turboprop Project written by Roy D. Hager and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1988 with Airplanes categories.
Low Speed Wind Tunnel Testing
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Author : Jewel B. Barlow
language : en
Publisher: John Wiley & Sons
Release Date : 1999-02-22
Low Speed Wind Tunnel Testing written by Jewel B. Barlow and has been published by John Wiley & Sons this book supported file pdf, txt, epub, kindle and other format this book has been release on 1999-02-22 with Technology & Engineering categories.
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.
Flight Stability And Automatic Control
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Author : Robert C. Nelson
language : en
Publisher: WCB/McGraw-Hill
Release Date : 1998
Flight Stability And Automatic Control written by Robert C. Nelson and has been published by WCB/McGraw-Hill this book supported file pdf, txt, epub, kindle and other format this book has been release on 1998 with Aerodynamique / Aeronautique / Aerospatial / Automatique / Avion / Commande / Conception / Controle / Navigation / Stabilite categories.
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.
Wind Tunnel Flight Correlation Of Shock Induced Separated Flow
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Author : Donald L. Loving
language : en
Publisher:
Release Date : 1966
Wind Tunnel Flight Correlation Of Shock Induced Separated Flow written by Donald L. Loving and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1966 with Aerodynamic load categories.
From Archangel To Senior Crown
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Author : Peter W. Merlin
language : en
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
Release Date : 2008
From Archangel To Senior Crown written by Peter W. Merlin and has been published by AIAA (American Institute of Aeronautics & Astronautics) this book supported file pdf, txt, epub, kindle and other format this book has been release on 2008 with History categories.
The Lockheed Blackbirds hold a unique place in the development of aeronautics. In their day, the A-12, YF-12, M-21, D-21, and SR-71 variants outperformed all other jet airplanes in terms of altitude and speed. Now retired, they remain the only production aircraft capable of sustained Mach 3 cruise and operational altitudes above 80,000 feet.This is the first book to address the technical aspects of these incredible aircraft. The author describes the design evolution of the Blackbird, from the Archangel to the Senior Crown (the Air Force's SR-71.) He describes in detail the construction and materials challenges faced by Lockheed, as well as the Blackbird's performance characteristics and capabilities.A NASA historian, the author describes NASA's role in using the aircraft as a flying laboratory to collect data on materials, structures, loads, heating, aerodynamics, and performance for high-speed aircraft. The reader will benefit from the technical and programmatic lessons learned.This volume was produced in cooperation with the National Aeronautics and Space Administration.