Aerodynamic Characteristics of a Model of a Proposed Six-Engine Hull-Type Seaplane at Mach Numbers of 1.57, 1.87, and 2.16

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ISBN 13 :
Total Pages : 42 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Aerodynamic Characteristics of a Model of a Proposed Six-Engine Hull-Type Seaplane at Mach Numbers of 1.57, 1.87, and 2.16 by : James R. Morgan

Download or read book Aerodynamic Characteristics of a Model of a Proposed Six-Engine Hull-Type Seaplane at Mach Numbers of 1.57, 1.87, and 2.16 written by James R. Morgan and published by . This book was released on 1960 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic and Hydrodynamic Characteristics of a Model of a 500,000-pound High-subsonic Multijet Logistics Transport Seaplane

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Publisher :
ISBN 13 :
Total Pages : 116 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Aerodynamic and Hydrodynamic Characteristics of a Model of a 500,000-pound High-subsonic Multijet Logistics Transport Seaplane by : Walter J. Kapryan

Download or read book Aerodynamic and Hydrodynamic Characteristics of a Model of a 500,000-pound High-subsonic Multijet Logistics Transport Seaplane written by Walter J. Kapryan and published by . This book was released on 1961 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.50 to 1.19 of a Supersonic Transport Model with a Modified M Wing

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Publisher :
ISBN 13 :
Total Pages : 84 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.50 to 1.19 of a Supersonic Transport Model with a Modified M Wing by : Edward J. Ray

Download or read book Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.50 to 1.19 of a Supersonic Transport Model with a Modified M Wing written by Edward J. Ray and published by . This book was released on 1967 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Static Aerodynamic Characteristics of a Model of a Typical Subsonic Jet-transport Airplane at Mach Numbers from 0.40 to 1.20

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Publisher :
ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Static Aerodynamic Characteristics of a Model of a Typical Subsonic Jet-transport Airplane at Mach Numbers from 0.40 to 1.20 by : Eugene N. Brooks

Download or read book Static Aerodynamic Characteristics of a Model of a Typical Subsonic Jet-transport Airplane at Mach Numbers from 0.40 to 1.20 written by Eugene N. Brooks and published by . This book was released on 1967 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Characteristics, Including Effect of Body Shape, of a Mach 6 Aircraft Concept

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ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Aerodynamic Characteristics, Including Effect of Body Shape, of a Mach 6 Aircraft Concept by : Gregory D. Riebe

Download or read book Aerodynamic Characteristics, Including Effect of Body Shape, of a Mach 6 Aircraft Concept written by Gregory D. Riebe and published by . This book was released on 1983 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Characteristics at Mach 6 of a Wing-body Concept for a Hypersonic Research Airplane

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Publisher :
ISBN 13 :
Total Pages : 68 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Aerodynamic Characteristics at Mach 6 of a Wing-body Concept for a Hypersonic Research Airplane by : James L. Dillon

Download or read book Aerodynamic Characteristics at Mach 6 of a Wing-body Concept for a Hypersonic Research Airplane written by James L. Dillon and published by . This book was released on 1978 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt: The static aerodynamic characteristics of a 1/30 scale model of a wing-body concept for a high speed research airplane were investigated in the Langley 20 inch Mach six tunnel. The investigation consisted of configuration buildup from the basic body by adding a wing, center vertical tail, three-module scramjet, and six-module scramjet engine. The test Mach number was six at a Reynolds number, based on model fuselage length, of about 13,700,000. The test angle-of-attack range was 4 to 20 D at constant angles of sideslip of 0, 2, and 4 deg. The elevons were deflected from 10 to -15 D for pitch control. Roll and yaw control were investigated. Experimental aerodynamic characteristics are compared with analytical elements.

Aerodynamic Characteristics at Mach 6 of a Hypersonic Research Airplane Concept Having a 70 ̊swept Delta Wing

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Publisher :
ISBN 13 :
Total Pages : 68 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Aerodynamic Characteristics at Mach 6 of a Hypersonic Research Airplane Concept Having a 70 ̊swept Delta Wing by : Louis E. Clark

Download or read book Aerodynamic Characteristics at Mach 6 of a Hypersonic Research Airplane Concept Having a 70 ̊swept Delta Wing written by Louis E. Clark and published by . This book was released on 1977 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Hydrodynamic Characteristics of a Model of a Proposed Six-engine Hull-type Sealane Designed for Supersonic Flight

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Publisher :
ISBN 13 :
Total Pages : 32 pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis Hydrodynamic Characteristics of a Model of a Proposed Six-engine Hull-type Sealane Designed for Supersonic Flight by : Claude W. Jr Coffee

Download or read book Hydrodynamic Characteristics of a Model of a Proposed Six-engine Hull-type Sealane Designed for Supersonic Flight written by Claude W. Jr Coffee and published by . This book was released on 1958 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Static Aerodynamic Characteristics at Mach Numbers from 2.50 to 4.63 of a Staged Airplane Model Designed for Cruise Above Mach 5

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ISBN 13 :
Total Pages : 62 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Static Aerodynamic Characteristics at Mach Numbers from 2.50 to 4.63 of a Staged Airplane Model Designed for Cruise Above Mach 5 by :

Download or read book Static Aerodynamic Characteristics at Mach Numbers from 2.50 to 4.63 of a Staged Airplane Model Designed for Cruise Above Mach 5 written by and published by . This book was released on 1964 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aircraft Design Projects

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Publisher : Elsevier
ISBN 13 : 0080498957
Total Pages : 393 pages
Book Rating : 4.0/5 (84 download)

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Book Synopsis Aircraft Design Projects by : Lloyd R. Jenkinson

Download or read book Aircraft Design Projects written by Lloyd R. Jenkinson and published by Elsevier. This book was released on 2003-04-28 with total page 393 pages. Available in PDF, EPUB and Kindle. Book excerpt: Written with students of aerospace or aeronautical engineering firmly in mind, this is a practical and wide-ranging book that draws together the various theoretical elements of aircraft design - structures, aerodynamics, propulsion, control and others - and guides the reader in applying them in practice. Based on a range of detailed real-life aircraft design projects, including military training, commercial and concept aircraft, the experienced UK and US based authors present engineering students with an essential toolkit and reference to support their own project work.All aircraft projects are unique and it is impossible to provide a template for the work involved in the design process. However, with the knowledge of the steps in the initial design process and of previous experience from similar projects, students will be freer to concentrate on the innovative and analytical aspects of their course project. The authors bring a unique combination of perspectives and experience to this text. It reflects both British and American academic practices in teaching aircraft design. Lloyd Jenkinson has taught aircraft design at both Loughborough and Southampton universities in the UK and Jim Marchman has taught both aircraft and spacecraft design at Virginia Tech in the US. * Demonstrates how basic aircraft design processes can be successfully applied in reality* Case studies allow both student and instructor to examine particular design challenges * Covers commercial and successful student design projects, and includes over 200 high quality illustrations

Aircraft Design

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Publisher : AIAA (American Institute of Aeronautics & Astronautics)
ISBN 13 : 9781563478291
Total Pages : 0 pages
Book Rating : 4.4/5 (782 download)

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Book Synopsis Aircraft Design by : Daniel P. Raymer

Download or read book Aircraft Design written by Daniel P. Raymer and published by AIAA (American Institute of Aeronautics & Astronautics). This book was released on 2006 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: Winner of the Summerfield Book Award Winner of the Aviation-Space Writers Association Award of Excellence. --Over 30,000 copies sold, consistently the top-selling AIAA textbook title This highly regarded textbook presents the entire process of aircraft conceptual designfrom requirements definition to initial sizing, configuration layout, analysis, sizing, and trade studiesin the same manner seen in industry aircraft design groups. Interesting and easy to read, the book has more than 800 pages of design methods, illustrations, tips, explanations, and equations, and extensive appendices with key data essential to design. It is the required design text at numerous universities around the world, and is a favorite of practicing design engineers.

Hydrodynamics of High-Speed Marine Vehicles

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Publisher : Cambridge University Press
ISBN 13 : 1139447939
Total Pages : 490 pages
Book Rating : 4.1/5 (394 download)

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Book Synopsis Hydrodynamics of High-Speed Marine Vehicles by : Odd M. Faltinsen

Download or read book Hydrodynamics of High-Speed Marine Vehicles written by Odd M. Faltinsen and published by Cambridge University Press. This book was released on 2006-01-09 with total page 490 pages. Available in PDF, EPUB and Kindle. Book excerpt: Hydrodynamics of High-Speed Marine Vehicles, first published in 2006, discusses the three main categories of high-speed marine vehicles - vessels supported by submerged hulls, air cushions or foils. The wave environment, resistance, propulsion, seakeeping, sea loads and manoeuvring are extensively covered based on rational and simplified methods. Links to automatic control and structural mechanics are emphasized. A detailed description of waterjet propulsion is given and the effect of water depth on wash, resistance, sinkage and trim is discussed. Chapter topics include resistance and wash; slamming; air cushion-supported vessels, including a detailed discussion of wave-excited resonant oscillations in air cushion; and hydrofoil vessels. The book contains numerous illustrations, examples and exercises.

The Evolution of the Cruise Missile

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Publisher :
ISBN 13 :
Total Pages : 308 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis The Evolution of the Cruise Missile by : Kenneth P. Werrell

Download or read book The Evolution of the Cruise Missile written by Kenneth P. Werrell and published by . This book was released on 1985 with total page 308 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Fox and McDonald's Introduction to Fluid Mechanics

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Publisher : John Wiley & Sons
ISBN 13 : 1119721024
Total Pages : 608 pages
Book Rating : 4.1/5 (197 download)

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Book Synopsis Fox and McDonald's Introduction to Fluid Mechanics by : Robert W. Fox

Download or read book Fox and McDonald's Introduction to Fluid Mechanics written by Robert W. Fox and published by John Wiley & Sons. This book was released on 2020-06-30 with total page 608 pages. Available in PDF, EPUB and Kindle. Book excerpt: Through ten editions, Fox and McDonald's Introduction to Fluid Mechanics has helped students understand the physical concepts, basic principles, and analysis methods of fluid mechanics. This market-leading textbook provides a balanced, systematic approach to mastering critical concepts with the proven Fox-McDonald solution methodology. In-depth yet accessible chapters present governing equations, clearly state assumptions, and relate mathematical results to corresponding physical behavior. Emphasis is placed on the use of control volumes to support a practical, theoretically-inclusive problem-solving approach to the subject. Each comprehensive chapter includes numerous, easy-to-follow examples that illustrate good solution technique and explain challenging points. A broad range of carefully selected topics describe how to apply the governing equations to various problems, and explain physical concepts to enable students to model real-world fluid flow situations. Topics include flow measurement, dimensional analysis and similitude, flow in pipes, ducts, and open channels, fluid machinery, and more. To enhance student learning, the book incorporates numerous pedagogical features including chapter summaries and learning objectives, end-of-chapter problems, useful equations, and design and open-ended problems that encourage students to apply fluid mechanics principles to the design of devices and systems.

Aviation Systems

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Publisher : Springer Science & Business Media
ISBN 13 : 364220080X
Total Pages : 247 pages
Book Rating : 4.6/5 (422 download)

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Book Synopsis Aviation Systems by : Andreas Wittmer

Download or read book Aviation Systems written by Andreas Wittmer and published by Springer Science & Business Media. This book was released on 2011-08-17 with total page 247 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book aims to provide comprehensive coverage of the field of air transportation, giving attention to all major aspects, such as aviation regulation, economics, management and strategy. The book approaches aviation as an interrelated economic system and in so doing presents the “big picture” of aviation in the market economy. It explains the linkages between domains such as politics, society, technology, economy, ecology, regulation and how these influence each other. Examples of airports and airlines, and case studies in each chapter support the application-oriented approach. Students and researchers in business administration with a focus on the aviation industry, as well as professionals in the industry looking to refresh or broaden their knowledge of the field will benefit from this book.

Probing the Sky

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Publisher :
ISBN 13 : 9781626830219
Total Pages : 334 pages
Book Rating : 4.8/5 (32 download)

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Book Synopsis Probing the Sky by : Curtis Peebles

Download or read book Probing the Sky written by Curtis Peebles and published by . This book was released on 2014-12-10 with total page 334 pages. Available in PDF, EPUB and Kindle. Book excerpt: With the development of supersonic aircraft, the X-plane era ushered in a new and challenging phase of flight. Researchers found that much of the knowledge accumulated from the previous, subsonic flight era did not apply to the emerging supersonic aircraft. These turbojet-powered planes also outpaced the usefulness of the wind tunnel, previously an indispensible tool of aeronautic research.This book explores the development of the X-series research aircraft, the planes that helped bridge the gap between subsonic flight and hypersonic flight.

Stratonauts

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Publisher : Springer Science & Business Media
ISBN 13 : 3319029010
Total Pages : 240 pages
Book Rating : 4.3/5 (19 download)

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Book Synopsis Stratonauts by : Manfred "Dutch" von Ehrenfired

Download or read book Stratonauts written by Manfred "Dutch" von Ehrenfired and published by Springer Science & Business Media. This book was released on 2013-12-13 with total page 240 pages. Available in PDF, EPUB and Kindle. Book excerpt: Just what does it take to be a stratonaut, soaring to higher and higher altitudes of Earth's atmosphere? Brave men and women have reached extreme heights in balloons, aircraft and rocket ships over the past two centuries, from the first untethered balloon flight to the first flights in the newly defined stratosphere, through to the present flights that continue to set new records. This book defines the altitudes related to the stratosphere, how it changes with latitude and the effects on ascending aviators. Also described is how over time technology enabled aircraft and balloons to achieve higher altitudes. The book shows the clear influence of the military on designs that initially focused on speed and maneuverability, but only later on reaching new altitudes. The early flights into the troposphere and eventually the mid to upper reaches of the stratosphere are chronicled, with great emphasis on flight operations. This includes decompression, bailouts, inertia coupling, ejections, catastrophic disintegration, crashes and deaths. Although the book highlights major altitude attempts and records, it also focuses on the life-threatening problems confronting the would-be stratonaut and the causes of many of their deaths. In doing so, it tries to define just what it takes to be a stratonaut.