Effects of Wing Inboard Plan-form Modifications on Lift, Drag, and Longitudinal Stability at Mach Numbers from 1.0 to 2.3 of a Rocket-propelled Free-flight Model with a 52.5 Degree Sweptback Wing of Aspect Ratio 3 PDF Download

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Effects of Wing Inboard Plan-form Modifications on Lift, Drag, and Longitudinal Stability at Mach Numbers from 1.0 to 2.3 of a Rocket-propelled Free-flight Model with a 52.5 Degree Sweptback Wing of Aspect Ratio 3

Effects of Wing Inboard Plan-form Modifications on Lift, Drag, and Longitudinal Stability at Mach Numbers from 1.0 to 2.3 of a Rocket-propelled Free-flight Model with a 52.5 Degree Sweptback Wing of Aspect Ratio 3 PDF Author: Allen B. Henning
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 32

Book Description
An investigation was made to determine the effects of wing inboard plan-form modifications on the lift, drag, and longitudinal characteristics of a rocket-propelled free-flight model. The model had a body of fineness ration 17.4, a modified wing with a basic plan form swept back 52.5 degrees and an aspect ratio of 3, and inline horizontal tail surfaces which were aerodynamically pulsed continuously throughout the flight.

Effects of Wing Inboard Plan-form Modifications on Lift, Drag, and Longitudinal Stability at Mach Numbers from 1.0 to 2.3 of a Rocket-propelled Free-flight Model with a 52.5 Degree Sweptback Wing of Aspect Ratio 3

Effects of Wing Inboard Plan-form Modifications on Lift, Drag, and Longitudinal Stability at Mach Numbers from 1.0 to 2.3 of a Rocket-propelled Free-flight Model with a 52.5 Degree Sweptback Wing of Aspect Ratio 3 PDF Author: Allen B. Henning
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 32

Book Description
An investigation was made to determine the effects of wing inboard plan-form modifications on the lift, drag, and longitudinal characteristics of a rocket-propelled free-flight model. The model had a body of fineness ration 17.4, a modified wing with a basic plan form swept back 52.5 degrees and an aspect ratio of 3, and inline horizontal tail surfaces which were aerodynamically pulsed continuously throughout the flight.

Flight Stability and Automatic Control

Flight Stability and Automatic Control PDF Author: Robert C. Nelson
Publisher:
ISBN:
Category : History
Languages : en
Pages : 464

Book Description
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.

Dynamics of Flight

Dynamics of Flight PDF Author: Bernard Etkin
Publisher: John Wiley & Sons
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 392

Book Description


Probing the Sky

Probing the Sky PDF Author: Curtis Peebles
Publisher:
ISBN: 9781626830219
Category : Research aircraft
Languages : en
Pages : 334

Book Description
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.

Airfoil Design and Data

Airfoil Design and Data PDF Author: Richard Eppler
Publisher: Springer Science & Business Media
ISBN: 3662026465
Category : Technology & Engineering
Languages : en
Pages : 569

Book Description
This detailed book describes a procedure for the design and analysis of subsonic airfoils. Contains 116 new airfoils for a wide range of Reynolds numbers and application requirements, including the input data for the computer code.

Aerodynamics of V/STOL Flight

Aerodynamics of V/STOL Flight PDF Author: Barnes Warnock McCormick
Publisher: Courier Corporation
ISBN: 9780486404608
Category : Technology & Engineering
Languages : en
Pages : 356

Book Description
An extremely practical overview of V/STOL (vertical/short takeoff and landing) aerodynamics, this volume offers a presentation of general theoretical and applied aerodynamic principles, covering propeller and helicopter rotor theory for both the static and forward flight cases. Both a text for students and a reference for professionals, the book can be used for advanced undergraduate or graduate courses. Numerous detailed figures, plus exercises. 1967 edition. Preface. Appendix. Index.

Aerodynamics, Aeronautics, and Flight Mechanics

Aerodynamics, Aeronautics, and Flight Mechanics PDF Author: Barnes W. McCormick
Publisher: John Wiley & Sons
ISBN: 0471575062
Category : Technology & Engineering
Languages : en
Pages : 677

Book Description
A New Edition of the Most Effective Text/Reference in the Field! Aerodynamics, Aeronautics, and Flight Mechanics, Second Edition Barnes W. McCormick, Pennsylvania State University 57506-2 When the first edition of Aerodynamics, Aeronautics, and Flight Mechanics was published, it quickly became one of the most important teaching and reference tools in the field. Not only did generations of students learn from it, they continue to use it on the job-the first edition remains one of the most well-thumbed guides you'll find in an airplane company. Now this classic text/reference is available in a bold new edition. All new material and the interweaving of the computer throughout make the Second Edition even more practical and current than before! A New Edition as Complete and Applied as the First Both analytical and applied in nature, Aerodynamics, Aeronautics, and Flight Mechanics presents all necessary derivations to understand basic principles and then applies this material to specific examples. You'll find complete coverage of the full range of topics, from aerodynamics to propulsion to performance to stability and control. Plus, the new Second Edition boasts the same careful integration of concepts that was an acclaimed feature of the previous edition. For example, Chapters 9, 10, and 11 give a fully integrated presentation of static, dynamic, and automatic stability and control. These three chapters form the basis of a complete course on stability and control. New Features You'll Find in the Second Edition * A new chapter on helicopter and V/STOL aircraft- introduces a phase of aerodynamics not covered in most current texts * Even more material than the previous edition, including coverage of stealth airplanes and delta wings * Extensive use of the computer throughout- each chapter now contains several computer exercises * A computer disk with programs written by the author is available

Theory of Wing Sections

Theory of Wing Sections PDF Author: Ira H. Abbott
Publisher: Courier Corporation
ISBN: 0486134997
Category : Technology & Engineering
Languages : en
Pages : 708

Book Description
Concise compilation of subsonic aerodynamic characteristics of NACA wing sections, plus description of theory. 350 pages of tables.

Lightning Protection of Aircraft

Lightning Protection of Aircraft PDF Author: Franklin Fisher
Publisher: CreateSpace
ISBN: 9781478241522
Category :
Languages : en
Pages : 564

Book Description
This book is an attempt to present under one cover the current state of knowledge concerning the potential lightning effects on aircraft and that means that are available to designers and operators to protect against these effects. The impetus for writing this book springs from two sources- the increased use of nonmetallic materials in the structure of aircraft and the constant trend toward using electronic equipment to handle flight-critical control and navigation function.

Design and Development of Aerospace Vehicles and Propulsion Systems

Design and Development of Aerospace Vehicles and Propulsion Systems PDF Author: S. Kishore Kumar
Publisher: Springer Nature
ISBN: 9811596018
Category : Technology & Engineering
Languages : en
Pages : 529

Book Description
This book presents selected papers presented in the Symposium on Applied Aerodynamics and Design of Aerospace Vehicles (SAROD 2018), which was jointly organized by Aeronautical Development Agency (the nodal agency for the design and development of combat aircraft in India), Gas-Turbine Research Establishment (responsible for design and development of gas turbine engines for military applications), and CSIR-National Aerospace Laboratories (involved in major aerospace programs in the country such as SARAS program, LCA, Space Launch Vehicles, Missiles and UAVs). It brings together experiences of aerodynamicists in India as well as abroad in Aerospace Vehicle Design, Gas Turbine Engines, Missiles and related areas. It is a useful volume for researchers, professionals and students interested in diversified areas of aerospace engineering.