Design Guide for Pitch-up Evaluation and Investigation at High Subsonic Speeds of Possible Limitations Due to Wing-aspect-ratio Variations PDF Download
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Author: Kenneth P. Spreemann
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 42
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Book Description
Author: Kenneth P. Spreemann
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 42
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Book Description
![Design Guide for Pitch-up Evaluation and Investigation at High Subsonic Speeds of Possible Limitations Due to Wing-aspect-ratio Variations [with List of References] PDF](https://books.google.com/books/content/images/frontcover/0e0otAEACAAJ?fife=w80-h100)
Author:
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Category :
Languages : en
Pages : 37
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Book Description
Author: Snorri Gudmundsson
Publisher: Butterworth-Heinemann
ISBN: 0128226471
Category : Business & Economics
Languages : en
Pages : 1146
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Book Description
General Aviation Aircraft Design, Second Edition, continues to be the engineer’s best source for answers to realistic aircraft design questions. The book has been expanded to provide design guidance for additional classes of aircraft, including seaplanes, biplanes, UAS, high-speed business jets, and electric airplanes. In addition to conventional powerplants, design guidance for battery systems, electric motors, and complete electric powertrains is offered. The second edition contains new chapters: Thrust Modeling for Gas Turbines Longitudinal Stability and Control Lateral and Directional Stability and Control These new chapters offer multiple practical methods to simplify the estimation of stability derivatives and introduce hinge moments and basic control system design. Furthermore, all chapters have been reorganized and feature updated material with additional analysis methods. This edition also provides an introduction to design optimization using a wing optimization as an example for the beginner. Written by an engineer with more than 25 years of design experience, professional engineers, aircraft designers, aerodynamicists, structural analysts, performance analysts, researchers, and aerospace engineering students will value the book as the classic go-to for aircraft design. The printed book is now in color, with 1011 figures and illustrations! Presents the most common methods for conceptual aircraft design Clear presentation splits text into shaded regions, separating engineering topics from mathematical derivations and examples Design topics range from the "new" 14 CFR Part 23 to analysis of ducted fans. All chapters feature updated material with additional analysis methods. Many chapters have been reorganized for further help. Introduction to design optimization is provided using a wing optimization as an example for the beginner Three new chapters are offered, two of which focus on stability and control. These offer multiple practical methods to simplify the estimation of stability derivatives. The chapters introduce hinge moments and basic control system design Real-world examples using aircraft such as the Cirrus SR-22 and Learjet 45
Author:
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ISBN:
Category : Government publications
Languages : en
Pages : 1878
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Book Description
Author: United States. Department of Commerce. Office of Technical Services
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 836
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Book Description
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1160
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Book Description
Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 548
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 464
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Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 244
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Book Description
Author: Robert J. Woodcock
Publisher:
ISBN:
Category : Aeroelasticity
Languages : en
Pages : 144
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Book Description
"Methods, ranging from rigorous and complicated to simple and approximate, are presented for estimating flying qualities in accordance with such specifications as MIL-F-8785 (ASG). Aerodynamic and inertial data are assumed to be known. Intended mainly for design use, the report gives enough detail to indicate derivations and conditions for validity. Topics include the static and dynamic, controls-fixed and controls-free aspects of aircraft stability, control, and trim. Although emphasis is on linear analysis, methods are given or indicated for such nonlinear problems as drag, pitch-up, inertial coupling, and spinning. Appendixes give an introduction to aeroelastic effects, ways to analyze control tabs, a derivation of the controls-free equations of motion, and an introduction to root locus analysis." -- page iii.
