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INTRODUCTION TO AIRCRAFT AEROELASTICITY AND LOADS

	Introduction To Aircraft Aeroelasticity And Loads by Jan Robert Wright, Jonathan Edward Cooper
	Price : Rs 1095.00
	Your Price : Rs 930.75

There is a need for a good textbook which covers the range of aero elastic and dynamic loads topics (whilst also providing an understanding of the principals involved) without the inclusion of complicated mathematics. Many tutors/lecturers in the field feel that it is not appropriate to give the ˜classical` books (published in the 50`s and 60`s) to new graduate engineers as they are too theoretical for novices, over length, out of date and not easily accessible. As an introduction to aircraft aero elasticity and dynamic loads, the proposed book should not only be welcomed by junior practitioners in industry and graduate students, it is also likely to form an excellent basis for several university courses on aero elasticity.Preface.
Introduction.
Abbreviations.

Part I: Background Material.
• Vibration of Single Degree of Freedom Systems.
• Vibration of Multiple Degree of Freedom Systems.
• Vibration of Continuous Systems - Assumed Shapes Approach.
• Vibration of Continuous Systems - Discretization Approach.
• Introduction to Steady Aerodynamics.
• Introduction to Loads.
• Introduction to Control.

Part II: Introduction to Aero elasticity and Loads.
• Static Aero elasticity - Effect of Wing Flexibility on Lift Distribution and Divergence.
• Static Aero elasticity - Effect of Wing Flexibility on Control Effectiveness.
• Introduction to Unsteady Aerodynamics.
• Dynamic Aero elasticity - Flutter.
• Aeroservoelasticity.
• Equilibrium Manoeuvres.
• Flight Mechanics Model for Dynamic Manoeuvres.
• Dynamic Manoeuvres.
• Gust and turbulence Encounters.
• Ground Manoeuvres.
• Aircraft Internal Loads.
• Potential Flow Aerodynamics.
• Coupling of Structural and Aerodynamic Computational Models.

Part III: Introduction to Industrial Practice.
• Aircraft Design and Certification.
• Aero elasticity and Loads Models.
• Static Aero elasticity and Flutter.
• Flight Manoeuvre and Gust/Turbulence Loads.
• Ground Manoeuvre Loads.
• Testing relevant to aero elasticity and Loads.

Appendices.
A. Aircraft Rigid Body Modes.
B. Table of Longitudinal Aerodynamic Derivatives.
C. Aircraft Symmetric Flexible Modes.
D. Model Condensation.
E. Aerodynamic Derivatives in body Fixed Axes.
F. Aircraft Antisymmetric Flexible Modes.
References.
Index.ISBN - 9788126548187

Pages : 528

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Introduction To Aircraft Aeroelasticity And Loads

by Jan Robert Wright, Jonathan Edward Cooper