Scientific and Technical Aerospace Reports

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Publisher :
ISBN 13 :
Total Pages : 1492 pages
Book Rating : 4.U/5 (183 download)

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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 1966 with total page 1492 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Stability and Control Characteristics at a Mach Number of 2.01 of a Variable-wing-sweep Configuration with Outboard Wing Panels Swept Back 75°

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Author :
Publisher :
ISBN 13 :
Total Pages : 26 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Stability and Control Characteristics at a Mach Number of 2.01 of a Variable-wing-sweep Configuration with Outboard Wing Panels Swept Back 75° by : M. Leroy Spearman

Download or read book Stability and Control Characteristics at a Mach Number of 2.01 of a Variable-wing-sweep Configuration with Outboard Wing Panels Swept Back 75° written by M. Leroy Spearman and published by . This book was released on 1959 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Stability and Control Characteristics at Mach Numbers of 2.50, 3.00, and 3.71 of a Variable- Wing-sweep Configuration with Outboard Wing Panels Swept Back 75°

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Publisher :
ISBN 13 :
Total Pages : 38 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Stability and Control Characteristics at Mach Numbers of 2.50, 3.00, and 3.71 of a Variable- Wing-sweep Configuration with Outboard Wing Panels Swept Back 75° by : Gerald V. Foster

Download or read book Stability and Control Characteristics at Mach Numbers of 2.50, 3.00, and 3.71 of a Variable- Wing-sweep Configuration with Outboard Wing Panels Swept Back 75° written by Gerald V. Foster and published by . This book was released on 1960 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Flight Stability and Automatic Control

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Publisher :
ISBN 13 :
Total Pages : 464 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Flight Stability and Automatic Control by : Robert C. Nelson

Download or read book Flight Stability and Automatic Control written by Robert C. Nelson and published by . This book was released on 1998 with total page 464 pages. Available in PDF, EPUB and Kindle. Book excerpt: This 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.

Stability and Control Characteristics at a Mach Number of 1.41 of a Variable-sweep Airplane Configuration Capable of Low-level Supersonic Attack-outer Wing Swept 75°and 108°

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Publisher :
ISBN 13 :
Total Pages : 32 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Stability and Control Characteristics at a Mach Number of 1.41 of a Variable-sweep Airplane Configuration Capable of Low-level Supersonic Attack-outer Wing Swept 75°and 108° by : Ross B. Robinson

Download or read book Stability and Control Characteristics at a Mach Number of 1.41 of a Variable-sweep Airplane Configuration Capable of Low-level Supersonic Attack-outer Wing Swept 75°and 108° written by Ross B. Robinson and published by . This book was released on 1960 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Sweeping Forward

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Publisher :
ISBN 13 : 9781626830080
Total Pages : 328 pages
Book Rating : 4.8/5 (3 download)

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Book Synopsis Sweeping Forward by :

Download or read book Sweeping Forward written by and published by . This book was released on 2013 with total page 328 pages. Available in PDF, EPUB and Kindle. Book excerpt: The X-29 was an unusual aircraft with a truly unique silhouette. It combined many features that challenged the technologies of its day and represented special problems for the developers and the team of testers responsible for documenting its features and design goals. This book is a look at the "big picture" of what this team accomplished in a relatively fast-paced test program involving the truly unique X-29.

Dynamics of Flight

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Publisher : John Wiley & Sons
ISBN 13 :
Total Pages : 392 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Dynamics of Flight by : Bernard Etkin

Download or read book Dynamics of Flight written by Bernard Etkin and published by John Wiley & Sons. This book was released on 1982 with total page 392 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Innovation in Flight

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Publisher :
ISBN 13 :
Total Pages : 406 pages
Book Rating : 4.3/5 ( download)

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Book Synopsis Innovation in Flight by : Joseph R. Chambers

Download or read book Innovation in Flight written by Joseph R. Chambers and published by . This book was released on 2005 with total page 406 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Rotary-Wing Aerodynamics

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Publisher : Courier Corporation
ISBN 13 : 0486318516
Total Pages : 640 pages
Book Rating : 4.4/5 (863 download)

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Book Synopsis Rotary-Wing Aerodynamics by : W. Z. Stepniewski

Download or read book Rotary-Wing Aerodynamics written by W. Z. Stepniewski and published by Courier Corporation. This book was released on 2013-04-22 with total page 640 pages. Available in PDF, EPUB and Kindle. Book excerpt: DIVClear, 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

Beyond Tube-and-Wing

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Publisher :
ISBN 13 : 9781626830592
Total Pages : pages
Book Rating : 4.8/5 (35 download)

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Book Synopsis Beyond Tube-and-Wing by : Bruce Larrimer

Download or read book Beyond Tube-and-Wing written by Bruce Larrimer and published by . This book was released on 2020-06-15 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.20 of a Variable-wing-sweep STOL Configuration

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Publisher :
ISBN 13 :
Total Pages : 32 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.20 of a Variable-wing-sweep STOL Configuration by : Gerald V. Foster

Download or read book Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.20 of a Variable-wing-sweep STOL Configuration written by Gerald V. Foster and published by . This book was released on 1960 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Columbia Crew Survival Investigation Report

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Publisher : PDQ Press
ISBN 13 : 9780979828898
Total Pages : 400 pages
Book Rating : 4.8/5 (288 download)

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Book Synopsis Columbia Crew Survival Investigation Report by : Nasa

Download or read book Columbia Crew Survival Investigation Report written by Nasa and published by PDQ Press. This book was released on 2009 with total page 400 pages. Available in PDF, EPUB and Kindle. Book excerpt: NASA commissioned the Columbia Accident Investigation Board (CAIB) to conduct a thorough review of both the technical and the organizational causes of the loss of the Space Shuttle Columbia and her crew on February 1, 2003. The accident investigation that followed determined that a large piece of insulating foam from Columbia's external tank (ET) had come off during ascent and struck the leading edge of the left wing, causing critical damage. The damage was undetected during the mission. The Columbia accident was not survivable. After the Columbia Accident Investigation Board (CAIB) investigation regarding the cause of the accident was completed, further consideration produced the question of whether there were lessons to be learned about how to improve crew survival in the future. This investigation was performed with the belief that a comprehensive, respectful investigation could provide knowledge that can protect future crews in the worldwide community of human space flight. Additionally, in the course of the investigation, several areas of research were identified that could improve our understanding of both nominal space flight and future spacecraft accidents. This report is the first comprehensive, publicly available accident investigation report addressing crew survival for a human spacecraft mishap, and it provides key information for future crew survival investigations. The results of this investigation are intended to add meaning to the sacrifice of the crew's lives by making space flight safer for all future generations.

Stability and Control Characteristics at Low Subsonic Speeds of an Airplane Configuration Having Two Types of Variable-sweep Wings

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Publisher :
ISBN 13 :
Total Pages : 98 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Stability and Control Characteristics at Low Subsonic Speeds of an Airplane Configuration Having Two Types of Variable-sweep Wings by : Bernard Spencer

Download or read book Stability and Control Characteristics at Low Subsonic Speeds of an Airplane Configuration Having Two Types of Variable-sweep Wings written by Bernard Spencer and published by . This book was released on 1960 with total page 98 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The Smell of Kerosene

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Publisher : DigiCat
ISBN 13 :
Total Pages : 276 pages
Book Rating : 4.8/5 (596 download)

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Book Synopsis The Smell of Kerosene by : National Aeronautics and Space Administration

Download or read book The Smell of Kerosene written by National Aeronautics and Space Administration and published by DigiCat. This book was released on 2022-11-13 with total page 276 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book puts the reader in the pilot's seat for a "day at the office" unlike any other. The Smell of Kerosene tells the dramatic story of a NASA research pilot who logged over 11,000 flight hours in more than 125 types of aircraft. Donald Mallick gives the reader fascinating first-hand description of his early naval flight training, carrier operations, and his research flying career with NASA. After transferring to the NASA Flight Research Center, Mallick became involved with projects that further pushed the boundaries of aerospace technology. These included the giant delta-winged XB-70 supersonic airplane, the wingless M2-F1 lifting body vehicle, and triple-sonic YF-12 Blackbird. Mallick also test flew the Lunar Landing Research Vehicle and helped develop techniques used in training astronauts to land on the Moon.

Wingless Flight

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Publisher : University Press of Kentucky
ISBN 13 : 9780813132228
Total Pages : 260 pages
Book Rating : 4.1/5 (322 download)

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Book Synopsis Wingless Flight by : R. Dale Reed, Darlene Lister

Download or read book Wingless Flight written by R. Dale Reed, Darlene Lister and published by University Press of Kentucky. This book was released on with total page 260 pages. Available in PDF, EPUB and Kindle. Book excerpt: "Much has been written about the famous conflicts and battlegrounds of the East during the American Revolution. Perhaps less familiar, but equally important and exciting, was the war on the western frontier, where Ohio Valley settlers fought for the land they had claimed -- and for their very lives. George Rogers Clark stepped forward to organize the local militias into a united front that would defend the western frontier from Indian attacks. Clark was one of the few people who saw the importance of the West in the war effort as a whole, and he persuaded Virginia's government to lend support to his efforts. As a result Clark was able to cross the Ohio, saving that part of the frontier from further raids. Lowell Harrison captures the excitement of this vital part of American history while giving a complete view of George Rogers Clark's significant achievements. Lowell H. Harrison, is a professor emeritus of history at Western Kentucky University and is the author or co-author of numerous books, including Lincoln of Kentucky, A New History of Kentucky, and Kentucky's Governors."

Effects of Spoiler-slot-deflector Control on the Aerodynamic Characteristics at a Mach Number of 2.01 of a Variable-wing-sweep Configuration with the Outer Wing Panels Swept Back 75°

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Publisher :
ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Effects of Spoiler-slot-deflector Control on the Aerodynamic Characteristics at a Mach Number of 2.01 of a Variable-wing-sweep Configuration with the Outer Wing Panels Swept Back 75° by : Gerald V. Foster

Download or read book Effects of Spoiler-slot-deflector Control on the Aerodynamic Characteristics at a Mach Number of 2.01 of a Variable-wing-sweep Configuration with the Outer Wing Panels Swept Back 75° written by Gerald V. Foster and published by . This book was released on 1960 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Natural Laminar Flow and Laminar Flow Control

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Publisher : Springer Science & Business Media
ISBN 13 : 1461228727
Total Pages : 415 pages
Book Rating : 4.4/5 (612 download)

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Book Synopsis Natural Laminar Flow and Laminar Flow Control by : R.W. Barnwell

Download or read book Natural Laminar Flow and Laminar Flow Control written by R.W. Barnwell and published by Springer Science & Business Media. This book was released on 2012-12-06 with total page 415 pages. Available in PDF, EPUB and Kindle. Book excerpt: Research on laminar flow and its transition to turbulent flow has been an important part of fluid dynamics research during the last sixty years. Since transition impacts, in some way, every aspect of aircraft performance, this emphasis is not only understandable but should continue well into the future. The delay of transition through the use of a favorable pressure gradient by proper body shaping (natural laminar flow) or the use of a small amount of suction (laminar flow control) was recognized even in the early 1930s and rapidly became the foundation of much of the laminar flow research in the U.S. and abroad. As one would expect, there have been many approaches, both theoretical and experimental, employed to achieve the substantial progress made to date. Boundary layer stability theories have been formu lated and calibrated by a good deal of wind tunnel and flight experiments. New laminar now airfoils and wings have been designed and many have been employed in aircraft designs. While the early research was, of necessity, concerned with the design of subsonic aircraft interest has steadily moved to higher speeds including those appropriate to planetary entry. Clearly, there have been substantial advances in our understanding of transition physics and in the development and application of transition prediction methodolo gies to the design of aircraft.