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(Ebook) Aircraft Performance and Design 1st Edition by J D Anderson ISBN 0070702454 9780070702455

  • SKU: EBN-10960350
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Authors:J. D. Anderson
Pages:596 pages.
Year:2010
Editon:Reprint
Publisher:McGraw-Hill Education (India) Pvt Limited
Language:english
File Size:16.46 MB
Format:pdf
ISBNS:9780070702455, 0070702454
Categories: Ebooks

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(Ebook) Aircraft Performance and Design 1st Edition by J D Anderson ISBN 0070702454 9780070702455

(Ebook) Aircraft Performance and Design 1st Edition by J D Anderson - Ebook PDF Instant Download/Delivery: 0070702454, 9780070702455
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ISBN 10: 0070702454 
ISBN 13: 9780070702455
Author: J D Anderson

John D. Anderson Jr.'s "Aircraft Performance & Design" is a well-regarded textbook that integrates both performance analysis and the design philosophy of aircraft. Based on various academic and publisher descriptions.

(Ebook) Aircraft Performance and Design 1st Table of contents:

Part I: Preliminary Considerations

  • Chapter 1: The Evolution of the Airplane and its Performance: A Short History

    • Early Developments and Pioneers

    • Key Historical Milestones in Aircraft Design and Performance

    • The Importance of Historical Context in Design

  • Chapter 2: Aerodynamics of the Airplane: The Drag Polar

    • Basic Aerodynamic Principles

    • Lift, Drag, and Moment

    • Airfoils and Wings

    • The Drag Polar and its Significance

    • Induced Drag, Parasite Drag, and Wave Drag

  • Chapter 3: Some Propulsion Characteristics

    • Types of Aircraft Propulsion Systems (Propeller, Jet Engines)

    • Thrust and Power Generation

    • Specific Fuel Consumption

    • Propeller Efficiency

    • Engine Performance Characteristics with Altitude and Speed

Part II: Airplane Performance: Static and Accelerated Flight

  • Chapter 4: The Equations of Motion

    • Derivation of Fundamental Equations of Motion for Aircraft

    • Forces Acting on an Aircraft in Flight

    • Coordinate Systems

  • Chapter 5: Airplane Performance: Steady Flight

    • Straight and Level Flight

    • Minimum Drag and Maximum Lift-to-Drag Ratio

    • Endurance and Range for Propeller-Driven Aircraft

    • Endurance and Range for Jet Aircraft

    • Glide Performance

    • Absolute Ceiling and Service Ceiling

  • Chapter 6: Airplane Performance: Accelerated Flight

    • Takeoff Performance (Ground Roll, Rotation, Climb to Obstacle Clearance)

    • Landing Performance (Approach, Flare, Ground Roll)

    • Climb Performance (Rate of Climb, Climb Angle, Time to Climb)

    • Descent Performance

    • Maneuver Performance (Turns, Pull-ups, Push-overs)

    • V-n Diagram (Flight Envelope)

    • Energy Concepts and Specific Excess Power

Part III: Airplane Design

  • Chapter 7: The Philosophy and Methodology of Aircraft Design

    • The Design Process: From Concept to Detailed Design

    • Design Requirements and Specifications

    • Iteration and Optimization in Design

    • Trade Studies

    • Importance of Synthesis and Analysis

  • Chapter 8: Design of a Propeller-Driven Airplane

    • Conceptual Design Process

    • Weight Estimation

    • Configuration Layout

    • Constraint Analysis and Sizing

    • Wing Loading and Thrust-to-Weight Ratio

    • Case Studies of Propeller Aircraft Design

  • Chapter 9: Design of Jet-Propelled Airplanes

    • Differences in Design Considerations for Jet Aircraft

    • High-Speed Aerodynamics

    • Engine-Airframe Integration

    • Supersonic Flight Considerations

    • Design Examples of Jet Aircraft

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Tags: J D Anderson, Aircraft, Performance

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