An Experimental Transonic Investigation of a 45© Sweptback Wing-body Combination with Several Types of Body Indentation with Theoretical Comparisons Included

An Experimental Transonic Investigation of a 45© Sweptback Wing-body Combination with Several Types of Body Indentation with Theoretical Comparisons Included PDF Author: Melvin M. Carmel
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 60

Book Description


Aerodynamics of Wings and Bodies

Aerodynamics of Wings and Bodies PDF Author: Holt Ashley
Publisher: Courier Corporation
ISBN: 0486648990
Category : Technology & Engineering
Languages : en
Pages : 306

Book Description
This excellent, innovative reference offers a wealth of useful information and a solid background in the fundamentals of aerodynamics. Fluid mechanics, constant density inviscid flow, singular perturbation problems, viscosity, thin-wing and slender body theories, drag minimalization, and other essentials are addressed in a lively, literate manner and accompanied by diagrams.

A Modern Course in Aeroelasticity

A Modern Course in Aeroelasticity PDF Author: E.H. Dowell
Publisher: Springer Science & Business Media
ISBN: 9401104999
Category : Technology & Engineering
Languages : en
Pages : 724

Book Description
Aeroelasticity is the study of flexible structures situated in a flowing fluid. Its modern origins are in the field of aerospace engineering, but it has now expanded to include phenomena arising in other fields such as bioengineering, civil engineering, mechanical engineering and nuclear engineering. The present volume is a teaching text for a first, and possibly second, course in aeroelasticity. It will also be useful as a reference source on the fundamentals of the subject for practitioners. In this third edition, several chapters have been revised and three new chapters added. The latter include a brief introduction to `Experimental Aeroelasticity', an overview of a frontier of research `Nonlinear Aeroelasticity', and the first connected, authoritative account of `Aeroelastic Control' in book form. The authors are drawn from a range of fields including aerospace engineering, civil engineering, mechanical engineering, rotorcraft and turbomachinery. Each author is a leading expert in the subject of his chapter and has many years of experience in consulting, research and teaching.

The Cutting Edge

The Cutting Edge PDF Author: Mark A. Lorell
Publisher: Rand Corporation
ISBN: 0833025953
Category : History
Languages : en
Pages : 247

Book Description
The proposition that innovation is critical in the cost-effective design and development of successful military aircraft is still subject to some debate. RAND research indicates that innovation is promoted by intense competition among three or more industry competitors. Given the critical policy importance of this issue in the current environment of drastic consolidation of the aerospace defense industry, the authors here examine the history of the major prime contractors in developing jet fighters since World War II. They make use of an extensive RAND database that includes nearly all jet fighters, fighter-attack aircraft, and bombers developed and flown by U.S. industry since 1945, as well as all related prototypes, modifications, upgrades, etc. The report concludes that (1) experience matters, because of the tendency to specialize and thus to develop system-specific expertise; (2) yet the most dramatic innovations and breakthroughs came from secondary or marginal players trying to compete with the industry leaders; and (3) dedicated military R&D conducted or directly funded by the U.S. government has been critical in the development of new higher-performance fighters and bombers.

A Modern Course in Aeroelasticity

A Modern Course in Aeroelasticity PDF Author: Robert Clark
Publisher: Springer Science & Business Media
ISBN: 9781402020391
Category : Mathematics
Languages : en
Pages : 788

Book Description
In this new edition, the fundamental material on classical linear aeroelasticity has been revised. Also new material has been added describing recent results on the research frontiers dealing with nonlinear aeroelasticity as well as major advances in the modelling of unsteady aerodynamic flows using the methods of computational fluid dynamics and reduced order modeling techniques. New chapters on aeroelasticity in turbomachinery and aeroelasticity and the latter chapters for a more advanced course, a graduate seminar or as a reference source for an entrée to the research literature.

Transonic Aerodynamic Loading Characteristics of a Wing-body-tail Combination Having 52.5° Sweptback Wing of Aspect Ratio 3 with Conical Wing Camber and Body Indentation for a Design Mach Number [square Root Of] 2

Transonic Aerodynamic Loading Characteristics of a Wing-body-tail Combination Having 52.5° Sweptback Wing of Aspect Ratio 3 with Conical Wing Camber and Body Indentation for a Design Mach Number [square Root Of] 2 PDF Author: Marlowe D. Cassetti
Publisher:
ISBN:
Category : Transonic wind tunnels
Languages : en
Pages : 104

Book Description
An investigation has been made of the effects of conical wing camber and body indentation according to the supersonic area rule on the aerodynamic wing loading characteristics of a wing-body-tail configuration at transonic speeds. The wing aspect ratio was 3, taper ratio was 0.1, and quarter-chord-line sweepback was 52.5° with 3-percent-thick airfoil sections. The tests were conducted in the Langley 16-foot transonic tunnel at Mach numbers from 0.80 to 1.05 and at angles of attack from 0° to 14°, with Reynolds numbers based on mean aerodynamic chord varying from 7 x 106 to 8 x 106. Conical camber delayed wing-tip stall and reduced the severity of the accompanying longitudinal instability but did not appreciably affect the spanwise load distribution at angles of attack below tip stall. Body indentation reduced to transonic chordwise center-of-pressure travel from about 8 percent to 5 percent of the mean aerodynamic chord.

Search and Rescue, Satellite System

Search and Rescue, Satellite System PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 8

Book Description


Strategic Air Warfare

Strategic Air Warfare PDF Author: Richard H. Kohn
Publisher: Air Force History & Museums Program
ISBN:
Category : History
Languages : en
Pages : 166

Book Description
The ability of the American air forces to wage war independently and to carry the battle to the enemy's heartland has played a critical role in American air doctrine and military strategy since the 1930s. Generals LeMay, Johnson, Burchinal, and Catton explain their roles in flying and commanding bombing missions and campaigns during World War II, in creating the atomic force in the immediate postwar years, and in building the Strategic Air Command in the 1950s. The Cuban Missile Crisis and the Vietnam War are also discussed.

Principles of Aeroelasticity

Principles of Aeroelasticity PDF Author: Raymond L. Bisplinghoff
Publisher: Courier Corporation
ISBN: 0486783162
Category : Technology & Engineering
Languages : en
Pages : 545

Book Description
Geared toward professional engineers, this volume will be helpful for students, too. Topics include methods of constructing static and dynamic equations, heated elastic solids, forms of aerodynamic operators, structural operators, and more. 1962 edition.

Influence of the Body Flow Field on the Zero-lift Wave Drag of Wing-body Combinations Modified in Accordance with the Transonic Area Rule

Influence of the Body Flow Field on the Zero-lift Wave Drag of Wing-body Combinations Modified in Accordance with the Transonic Area Rule PDF Author: William A. Page
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 32

Book Description