Longitudinal Stability and Trim of Two Rocket-propelled Airplane Models Having 45© Sweptback Wings and Tails with the Horizontal Tail Mounted in Two Positions

Longitudinal Stability and Trim of Two Rocket-propelled Airplane Models Having 45© Sweptback Wings and Tails with the Horizontal Tail Mounted in Two Positions PDF Author: James H. Parks
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 36

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Airplane Stability and Control

Airplane Stability and Control PDF Author: Malcolm J. Abzug
Publisher: Cambridge University Press
ISBN: 1107320194
Category : Technology & Engineering
Languages : en
Pages : 417

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Book Description
From the early machines to today's sophisticated aircraft, stability and control have always been crucial considerations. In this second edition, Abzug and Larrabee again forge through the history of aviation technologies to present an informal history of the personalities and the events, the art and the science of airplane stability and control. The book includes never-before-available impressions of those active in the field, from pre-Wright brothers airplane and glider builders through to contemporary aircraft designers. Arranged thematically, the book deals with early developments, research centers, the effects of power on stability and control, the discovery of inertial coupling, the challenge of stealth aerodynamics, a look toward the future, and much more. It is profusely illustrated with photographs and figures, and includes brief biographies of noted stability and control figures along with a core bibliography. Professionals, students, and aviation enthusiasts alike will appreciate this readable history of airplane stability and control.

Dark Eagles

Dark Eagles PDF Author: Curtis Peebles
Publisher: iBooks
ISBN: 9780743458368
Category : Aeronautics, Military
Languages : en
Pages : 0

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Book Description
This extraordinary history of the nation's top-secret military aircraft spans from World War II to the Gulf War, and chronicles how these planes--called "Dark Eagles" because they were painted black--were developed, tested, and operated in secrecy.

Aircraft Dynamic Stability and Response

Aircraft Dynamic Stability and Response PDF Author: A. W. Babister
Publisher: Elsevier
ISBN: 1483140350
Category : Technology & Engineering
Languages : en
Pages : 247

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Book Description
Aircraft Dynamic Stability and Response deals with the fundamentals of dynamic stability in aircraft. Topics covered include flight dynamics, equations of motion, and lateral and longitudinal aerodynamic derivatives. Basic lateral and longitudinal motions are also considered. A non-dimensional system of notation is used, and problems are included at the end of chapters. This book is comprised of 13 chapters and begins with an introduction to aircraft static stability and maneuverability, with emphasis on the theoretical basis of flight dynamics and the technical terms used. The physical background for the estimation of aerodynamic derivatives is discussed. Subsequent chapters focus on the longitudinal and lateral motion of aircraft, including the effect of automatic control; modern developments such as the effects of aeroelasticity, dynamic coupling, and high incidence; and aircraft response to gusts. The final chapter demonstrates how to estimate the aerodynamic derivatives, and hence the dynamic stability characteristics, of a typical fighter aircraft. Throughout the text, the aircraft and its behavior are kept well to the fore. This monograph is intended for undergraduate students of aeronautical engineering and for newcomers to the aircraft industry.

U.S. Standard Atmosphere Supplements, 1966

U.S. Standard Atmosphere Supplements, 1966 PDF Author: United States Committee on Extension to the Standard Atmosphere
Publisher:
ISBN:
Category : Standard atmosphere
Languages : en
Pages : 318

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Introduction to Aerodynamics

Introduction to Aerodynamics PDF Author: Gale M. Craig
Publisher:
ISBN: 9780964680630
Category : Aerodynamics
Languages : en
Pages : 214

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Longitudinal Stability Characteristics at Transonic Speeds of a Rocket-propelled Model of an Airplane Having a 45 Degree Swept Wing of Aspect Ratio 6.0

Longitudinal Stability Characteristics at Transonic Speeds of a Rocket-propelled Model of an Airplane Having a 45 Degree Swept Wing of Aspect Ratio 6.0 PDF Author: John C. McFall
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 44

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Aircraft

Aircraft PDF Author: DK
Publisher: National Geographic Books
ISBN: 0744027454
Category : Transportation
Languages : en
Pages : 0

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Book Description
Take an action-packed flight through the history of aircraft and discover the intrepid pioneers who made a dream reality Uncover the engineering behind more than 800 aircraft models, from military jets to commercial planes. This visual history book captures the fascinating story of airplanes and aviation, and how their groundbreaking discovery has influenced the 21st Century. Inside the pages of this aircraft book, you’ll discover: • The history of military and commercial aircraft from all over the world, decade by decade, to the present day in stunning visual detail • Comprehensive catalogs highlight the most important aircraft of each period along with their specifications and unique features • Showcases on particularly celebrated aircraft – such as the Supermarine Spitfire and Concorde – in beautifully photographed “virtual tour” features • The stories of the engineers and manufacturers that created marques like Boeing and Airbus Take to the skies Modern flight has opened the world up to new opportunities and paved the way for the development of advanced research and technology. But, what made it so groundbreaking? This book uncovers the stories behind the first airplane models, the development of flight, and brings you to present-day marvels such as the Gypsy Moth and Supermarine Spitfire. The Aircraft Book is filled with stats, facts, and photographs that create a visual tour and allows you to see inside key commercial and military aircraft models from the exterior to the cockpit. Aviation enthusiasts will also be captivated by the manufacturer of aircraft engines and how famous models like Boeing and Lockheed became household names. Love history? Discover even more with DK! DK's The Definitive Visual History series is an iconic celebration of design and history. Packed with fascinating facts and statistics, these high-quality visual guides cover everything from history and notable designs to the people and technology that made it possible. Books in this series include The Car Book, The Train Book, The Tank Book, and so much more.

Special Course on Aircraft Dynamics at High Angles of Attack: Experiments and Modelling

Special Course on Aircraft Dynamics at High Angles of Attack: Experiments and Modelling PDF Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel. Special Course
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 154

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Book Description
"This report consists of lecture notes of an AGARD Fluid Dynamics Panel Special Course. These notes provide the latest information on the development and use of dynamic experiments in wind tunnels from several of the NATO nations. They address current oscillatory and rotary test techniques, experimental results for typical configurations, and the use of these data for flight mechanics applications. Subject included are: dynamic lift, wing rock, fluid dynamics of rotary flows, mathematical modelling, non-linear data representation, vortex manipulation for control enhancement, and correlations of predictions based on rotary and oscillatory wind-tunnel and flight-test results. The complete course notes are contained in two volumes. The main part of the notes is contained in AGARD Advisory Report 265 (ADA235179). The present volume includes papers on: Unsteady aerodynamics of slender wings; Dynamic stall effects and applications to high performance aircraft; Oscillatory test techniques; Large amplitude oscillations; Oscillatory data for typical configurations; and Forebody vortex control."--Stinet.

Effect of Horizontal-tail Location on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45° Sweptback Wing and Tail Surfaces

Effect of Horizontal-tail Location on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45° Sweptback Wing and Tail Surfaces PDF Author: Jacob H. Lichtenstein
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 34

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Book Description
Wind-tunnel results are presented to show the effect of changes in horizontal-tail location on the low-speed static longitudinal stability and steady-state rotary damping in pitch for a complete model with wing and tail surfaces having the quarter-chord lines swept back 45 degrees.