General Aviation Aircraft Design
Applied Methods and Procedures
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54 747 Ft (52 140 Ft + 5% VAT)
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54 747 Ft
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Out of print
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Delivery time is estimated on our previous experiences. We give estimations only, because we order from outside Hungary, and the delivery time mainly depends on how quickly the publisher supplies the book. Faster or slower deliveries both happen, but we do our best to supply as quickly as possible.
Product details:
- Publisher Elsevier Science
- Date of Publication 5 May 2016
- ISBN 9780128099988
- Binding Paperback
- No. of pages1048 pages
- Size 276x215 mm
- Weight 2490 g
- Language English 0
Categories
Long description:
"Find the right answer the first time with this useful handbook of preliminary aircraft design. Written by an engineer with close to 20 years of design experience, General Aviation Aircraft Design: Applied Methods and Procedures provides the practicing engineer with a versatile handbook that serves as the first source for finding answers to realistic aircraft design questions. The book is structured in an ""equation/derivation/solved example"" format for easy access to content. Readers will find it a valuable guide to topics such as sizing of horizontal and vertical tails to minimize drag, sizing of lifting surfaces to ensure proper dynamic stability, numerical performance methods, and common faults and fixes in aircraft design. In most cases, numerical examples involve actual aircraft specs. Concepts are visually depicted by a number of useful black-and-white figures, photos, and graphs (with full-color images included in the eBook only). Broad and deep in coverage, it is intended for practicing engineers, aerospace engineering students, mathematically astute amateur aircraft designers, and anyone interested in aircraft design."
MoreTable of Contents:
Introduction Aircraft Structural Layout The Power Plant Fluid Mechanics Trade Studies Aircraft Weight Analysis The Wing Planform The Anatomy of the Airfoil The Anatomy of the Wing Aircraft Drag Analysis The Propeller Tail Design Performance: Take-off Performance: Climb Performance: Cruise Performance: Range Analysis Performance: Descent Performance: Landing Static Longitudinal Stability Dynamic Longitudinal Stability Static Lateral and Directional Stability Dynamic Lateral and Directional Stability Control System Design Fuselage Design Miscellaneous Design Notes Aircraft Load Analysis Appendix A: Mathematics Appendix B: Physics
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