BESCHRIJVING Elements of airplane performance, 2nd edition This book contains sixteen chapters and four appendices which form a compre-hensive teaching text on the subject of airplane performance. The fi rst seven chapters are designed to provide necessary background material in mechanics, aerodynamics, atmospheric science, air data instruments, and propulsion. In addi-tion, the appendices furnish basic data and information on the theory pertinent to a clear understanding of the different problems. Chapters 8-13, in particular, treat the point performance of the airplane, i.e., the performance that pertain to given point on the fl ight path. Finally, chapters 14-16 deal with what is known as the integral performance, indicating the performance items which are related to the course of the fl ight.

1. Airplane Performance Data

The text is extensively illustrated and includes numerous worked examples. The book is primarily intended to serve as a textbook in undergraduate engineering courses and as an instrument for selfstudy.

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Contents Preface 1. Basic concepts 2. The atmosphere 3.

Equations of motion 4. Aerodynamic basis 5.

Airplane Performance Data

Air data instruments 6. Propulsion 7. Propeller perform-ance 8. The airplane in symmetric fl ight 9. Performance in steady symmetric fl ight 10. Effect of altitude 11. Flight and airplane condition effects 12.

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Turning performance 13. Gliding fl ight 14. Symmetric climb and descent 15. Cruise performance 16. Airfi eld performance References Appendix A. Newtonian mechanics Appendix B. Conversion factors Appendix C.

International standard atmosphere Appendix D. One-dimensional steady fl ow equations Index The author, Ger J.J. Ruijgrok, is an Emeritus Professor of Aerospace Engineering at the Brussels Free University (VUB), Belgium, and at the Delft University of Tech-nology, The Netherlands. He is also the author of the books Elements of Aviation Acoustics and Elements of Aircraft Pollution.

He was graduated at Delft University of Technology with a degree in aeronautical engineering. URL on this book: http://www.vssd.nl/hlf/ae02.htm.

Advanced Flight Dynamics With Elements Of Flight Control by / / / PDF Read Online Advanced Flight Dynamics aim to integrate the subjects of aircraft performance, trim and stability/control in a seamless manner. Advanced Flight Dynamics highlights three key and unique viewpoints. Firstly, it follows the revised and corrected aerodynamic modeling presented previously in recent textbook on Elementary Flight Dynamics. Secondly, it uses bifurcation and continuation theory, especially the Extended Bifurcation Analysis (EBA) procedure devised by the authors, to blend the subjects of aircraft performance, trim and stability, and flight control into a unified whole. Thirdly, rather than select one control design tool or another, it uses the generalized Nonlinear Dynamic Inversion (NDI) methodology to illustrate the fundamental principles of flight control. Advanced Flight Dynamics covers all the standard airplane maneuvers, various types of instabilities normally encountered in flight dynamics and illustrates them with real-life airplane data and examples, thus bridging the gap between the teaching of flight dynamics/ control theory in the university and its practice in airplane design bureaus.

The expected reader group for this book would ideally be senior undergraduate and graduate students, practicing aerospace/flight simulation engineers/scientists from industry as well as researchers in various organizations. Key Features: Focus on unified nonlinear approach, with nonlinear analysis tools. Provides an up-to-date, corrected, and unified presentation of aircraft trim, stability and control analysis including nonlinear phenomena and closed-loop stability analysis. Contains a computational tool and real-life example carried through the chapters. Includes complementary nonlinear dynamic inversion control approach, with relevant aircraft examples. Fills the gap in the market for a text including non-linear flight dynamics and continuation methods.