NASA Scientific and Technical Reports
Author | : United States. National Aeronautics and Space Administration Scientific and Technical Information Division |
Publisher | : |
Total Pages | : 1440 |
Release | : 1966 |
Genre | : Aeronautics |
ISBN | : |
Download Effects Of Wing Incidence On The Longitudinal Trim Characteristics Of A Cambered 70 Deg Delta Wing Configuration At Mach Numbers 30 To 50 full books in PDF, epub, and Kindle. Read online free Effects Of Wing Incidence On The Longitudinal Trim Characteristics Of A Cambered 70 Deg Delta Wing Configuration At Mach Numbers 30 To 50 ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Author | : United States. National Aeronautics and Space Administration Scientific and Technical Information Division |
Publisher | : |
Total Pages | : 1440 |
Release | : 1966 |
Genre | : Aeronautics |
ISBN | : |
Author | : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division |
Publisher | : |
Total Pages | : 1680 |
Release | : 1965 |
Genre | : Aeronautics |
ISBN | : |
Author | : Robert C. Nelson |
Publisher | : |
Total Pages | : 464 |
Release | : 1998 |
Genre | : History |
ISBN | : |
This edition of this this flight stability and controls guide features an unintimidating math level, full coverage of terminology, and expanded discussions of classical to modern control theory and autopilot designs. Extensive examples, problems, and historical notes, make this concise book a vital addition to the engineer's library.
Author | : Thomas R. Yechout |
Publisher | : AIAA |
Total Pages | : 666 |
Release | : 2003 |
Genre | : Aerodynamics |
ISBN | : 9781600860782 |
Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.
Author | : W. Z. Stepniewski |
Publisher | : Courier Corporation |
Total Pages | : 640 |
Release | : 2013-04-22 |
Genre | : Technology & Engineering |
ISBN | : 0486318516 |
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
Author | : |
Publisher | : |
Total Pages | : 748 |
Release | : 1965 |
Genre | : Government reports announcements & index |
ISBN | : |
Author | : Snorri Gudmundsson |
Publisher | : Butterworth-Heinemann |
Total Pages | : 1058 |
Release | : 2013-09-03 |
Genre | : Technology & Engineering |
ISBN | : 0123973295 |
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. - Organized by articles and structured in an "equation/derivation/solved example" format for easy access to the content you need - Numerical examples involve actual aircraft specs - Contains high-interest topics not found in other texts, including 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 - Provides a unique safety-oriented design checklist based on industry experience - Discusses advantages and disadvantages of using computational tools during the design process - Features detailed summaries of design options detailing the pros and cons of each aerodynamic solution - Includes three case studies showing applications to business jets, general aviation aircraft, and UAVs - Numerous high-quality graphics clearly illustrate the book's concepts (note: images are full-color in eBook only)
Author | : Ira H. Abbott |
Publisher | : Courier Corporation |
Total Pages | : 708 |
Release | : 2012-04-26 |
Genre | : Technology & Engineering |
ISBN | : 0486134997 |
Concise compilation of subsonic aerodynamic characteristics of NACA wing sections, plus description of theory. 350 pages of tables.