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Rotary-Wing Aerodynamics Revised Edition
Contributor(s): Stepniewski, W. Z. (Author)
ISBN: 0486646475     ISBN-13: 9780486646473
Publisher: Dover Publications
OUR PRICE:   $28.45  
Product Type: Paperback - Other Formats
Published: July 1984
Qty:
Temporarily out of stock - Will ship within 2 to 5 weeks
Annotation: Clear, 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.

Additional Information
BISAC Categories:
- Science
- Technology & Engineering | Aeronautics & Astronautics
Dewey: 629.132
LCCN: 83020528
Series: Engineering Series
Physical Information: 1.29" H x 6.13" W x 9.23" (1.90 lbs) 640 pages
 
Descriptions, Reviews, Etc.
Publisher Description:
Recent literature related to rotary-wing aerodynamics has increased geometrically; yet, the field has long been without the benefit of a solid, practical basic text. To fill that void in technical data, NASA (National Aeronautics and Space Administration) commissioned the highly respected practicing engineers and authors W. Z. Stepniewski and C. N. Keys to write one. The result: Rotary-Wing Aerodynamics, a clear, concise introduction, highly recommended by U.S. Army experts, that provides students of helicopter and aeronautical engineering with an understanding of the aerodynamic phenomena of the rotor. In addition, it furnishes the tools for quantitative evaluation of both rotor performance and the helicopter as a whole. Now both volumes of the original have been reprinted together in this inexpensive Dover edition.
In Volume I: "Basic Theories of Rotor Aerodynamics," the concept of rotary-wing aircraft in general is defined, followed by comparison of the energy effectiveness of helicopters with that of other static-thrust generators in hover, as well as with various air and ground vehicles in forward translation. Volume II: "Performance Prediction of Helicopters" offers practical application of the rotary-wing aerodynamic theories discussed in Volume I, and contains complete and detailed performance calculations for conventional single-rotor, winged, and tandem-rotor helicopters.
Graduate students with some background in general aerodynamics, or those engaged in other fields of aeronautical or nonaeronautical engineering, will find this an essential and thoroughly practical reference text on basic rotor dynamics. While the material deals primarily with the conventional helicopter and its typical regimes of flight, Rotary-Wing Aerodynamics also provides a comprehensive insight into other fields of rotary-wing aircraft analysis as well.