Author: Snorri Gudmundsson
Publisher: Butterworth-Heinemann
ISBN: 0128226471
Category : Business & Economics
Languages : en
Pages : 1146
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
General Aviation Aircraft Design
Aeronautical Engineering Review
Aerospace Vehicle Design: Aircraft design
Author: Karl Dawson Wood
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 504
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 504
Book Description
Summary of Low Speed Airfoil Data
Author: Michael S. Selig
Publisher: Soartech
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 320
Book Description
Publisher: Soartech
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 320
Book Description
Aerospace Engineering Index
Fowler Flaps for Airplanes
Author: Harlan D. Fowler
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 104
Book Description
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 104
Book Description
Aeronautical Engineering Index
Battelle Technical Review
Author: Battelle Memorial Institute
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 830
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 830
Book Description
Aerofoil Sections
Author: Friedrich Wilhelm Riegels
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 281
Book Description
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 281
Book Description
Aerodynamic Characteristics of the NACA 747A315 and 747A415 Airfoils from Tests in the NACA Two-dimensional Low-turbulence Pressure Tunnel
Author: Albert E. Von Doenhoff
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 24
Book Description
Summary: Two low-drag airfoils, the NACA 747A315 and the NACA 747A415, designed to have reduced pitching moments about the quarter-chord point and moderately high values of the design lift coefficient have been tested in the NACA two-dimensional low-turbulence pressure tunnel. Section lift, drag, and pitching-moment coefficients are presented for Reynolds numbers of 3 x 106, 6 x 106, and 9 x 106, together with section lift and section drag data for a Reynolds number of 6 x 106 for the same airfoils with roughened leading edges.
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 24
Book Description
Summary: Two low-drag airfoils, the NACA 747A315 and the NACA 747A415, designed to have reduced pitching moments about the quarter-chord point and moderately high values of the design lift coefficient have been tested in the NACA two-dimensional low-turbulence pressure tunnel. Section lift, drag, and pitching-moment coefficients are presented for Reynolds numbers of 3 x 106, 6 x 106, and 9 x 106, together with section lift and section drag data for a Reynolds number of 6 x 106 for the same airfoils with roughened leading edges.