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Rotary-Wing Aerodynamics

Rotary-Wing Aerodynamics
Author: W. Z. Stepniewski
Publisher: Courier Corporation
Total Pages: 640
Release: 2013-04-22
Genre: Technology & Engineering
ISBN: 0486318516

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DIVClear, concise text covers aerodynamic phenomena of the rotor and offers guidelines for helicopter performance evaluation. Originally prepared for NASA. Prefaces. New Indexes. 10 black-and-white photos. 537 figures. /div


Rotary-wing Aerodynamics

Rotary-wing Aerodynamics
Author: Wieslaw Zenon Stepniewski
Publisher: Courier Corporation
Total Pages: 640
Release: 1984-01-01
Genre: Technology & Engineering
ISBN: 0486646475

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Lærebogsagtig beskrivelse af de grundlæggende principper ved konstruktionen af helikoptere samt helikopterens særlige egenskaber


Rotary Wing Aerodynamics

Rotary Wing Aerodynamics
Author: W.Z. Stepniewski
Publisher:
Total Pages: 359
Release: 1979
Genre:
ISBN:

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Rotary-wing Aerodynamics

Rotary-wing Aerodynamics
Author: Wieslaw Zenon Stepniewski
Publisher:
Total Pages:
Release: 1984
Genre: Helicopters
ISBN: 9781523109562

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Rotary-wing Aerodynamics

Rotary-wing Aerodynamics
Author: Wieslaw Zenon Stepniewski
Publisher:
Total Pages:
Release: 1981
Genre:
ISBN:

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Fixed and Flapping Wing Aerodynamics for Micro Air Vehicle Applications

Fixed and Flapping Wing Aerodynamics for Micro Air Vehicle Applications
Author: Thomas J. Mueller
Publisher: AIAA
Total Pages: 614
Release: 2001
Genre: Aerodynamics
ISBN: 9781600864469

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This title reports on the latest research in the area of aerodynamic efficency of various fixed-wing, flapping wing, and rotary wing concepts. It presents the progress made by over fifty active researchers in the field.


Rotary Wing Structural Dynamics and Aeroelasticity

Rotary Wing Structural Dynamics and Aeroelasticity
Author: Richard L. Bielawa
Publisher: Amer Inst of Aeronautics &
Total Pages: 562
Release: 1992-01-01
Genre: Aeroelasticity.
ISBN: 9781563470318

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Drawing on his extensive experience as a practicing engineer, designer, educator, and researcher in rotorcraft, the author presents a comprehensive account of the fundamental concepts of structural dynamics and aeroelasticity for conventional rotary wing aircraft, as well as for the newly emerging tilt-rotor and tilt-wing concepts. Intended for use in graduate-level courses and by practicing engineers, the volume covers all of the important topics needed for the complete understanding of rotorcraft structural dynamics and aeroelasticity, including basic analysis tools, rotating beams, gyroscopic phenomena, drive system dynamics, fuselage vibrations, methods for controlling vibrations, dynamic test procedures, stability analysis, mechanical and aeromechanical instabilities of rotors and rotor-pylon assemblies, unsteady aerodynamics and flutter of rotors, and model testing. The text is further enhanced by the inclusion of problems in each chapter.