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230808 ||| eng |
| 020 |
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|a 1466566353
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| 020 |
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|a 9781466566354
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| 050 |
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4 |
|a TL716
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| 100 |
1 |
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|a Venkatesan, C.
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| 245 |
0 |
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|a Fundamentals of helicopter dynamics
|c C. Venkatesan
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| 260 |
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|a Boca Raton
|b CRC Press
|c 2015
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| 300 |
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|a xx, 318 pages .
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| 505 |
0 |
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|a Historical development of helicopters and overview -- Introduction to hovering and vertical flight theory -- Introduction to forward flight theory -- Rotor blade flapping motion: simple model -- Helicopter trim (or equilibrium) analysis -- Isolated rotor blade dynamics -- Rotor blade aeroelastic stability: coupled mode dynamics -- Rotor modes: multi-blade coordinate transformation -- Flap dynamics under general motion of the hub -- Helicopter stability and control -- Ground resonance-aeromechanical instability: a simple model
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| 505 |
0 |
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|a Includes bibliographical references (pages 305-309) and index
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| 653 |
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|a Helicopters / Aerodynamics / http://id.loc.gov/authorities/subjects/sh85060008
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| 653 |
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|a Rotors / Dynamics / http://id.loc.gov/authorities/subjects/sh85115508
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| 653 |
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|a Hélicoptères / Aérodynamique
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| 653 |
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|a Rotors / Dynamics / fast
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| 653 |
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|a TECHNOLOGY & ENGINEERING / Engineering (General) / bisacsh
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| 653 |
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|a SCIENCE / Mechanics / General / bisacsh
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| 653 |
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|a Helicopters / Aerodynamics / fast
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| 653 |
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|a TECHNOLOGY & ENGINEERING / Mechanical / bisacsh
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| 653 |
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|a TECHNOLOGY & ENGINEERING / Electrical / bisacsh
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| 041 |
0 |
7 |
|a eng
|2 ISO 639-2
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| 989 |
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|b OREILLY
|a O'Reilly
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| 776 |
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|z 9781466566354
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| 776 |
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|z 9781466566347
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| 776 |
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|z 1466566345
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| 776 |
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|z 1466566353
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| 856 |
4 |
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|u https://learning.oreilly.com/library/view/~/9781466566347/?ar
|x Verlag
|3 Volltext
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| 082 |
0 |
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|a 629.132/3
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| 082 |
0 |
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|a 500
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| 082 |
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|a 620
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| 520 |
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|a "This is an introductory book on helicopter dynamics. The aim of this book is to introduce the students/engineers to the basic principles of helicopter dynamics. The book focuses on three major topics: (i) rotor blade idealization and blade dynamics in flap, lag and torsion modes; (ii) rotor blade aeroelastic stability {coupled flap-lag and coupled flap-torsion}; (iii) coupled rotor-fuselage dynamics. It covers hover, forward flight and other manoeuvre flights. Starting from basic physics of rotating systems, the equations of motion have been derived in vector form."
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