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Aircraft design : a conceptual approach / Daniel P. Raymer.

By: Contributor(s): Material type: TextTextSeries: AIAA education seriesPublication details: Reston, Va. : American Institute of Aeronautics and Astronautics, 2006.Edition: 4th edDescription: xix, 838 p. : ill. ; 24 cmISBN:
  • 9781563478291:
  • 1563478293
Subject(s): DDC classification:
  • 629.1341
LOC classification:
  • .R29 2006
Contents:
Design - A Separate Discipline -- Overview of the Design Process -- Sizing from a Conceptual Sketch -- Airfoil and Geometry Selection -- Thrust-to-Weight Ratio and Wing Loading -- Initial Sizing -- Configuration Layout and Loft -- Special Considerations in Configuration Layout -- Crew Station, Passengers, and Payload -- Propulsion and Fuel System Integration -- Landing Gear and Subsystems -- Intermission: Step-by-Step Development of a New Design -- Aerodynamics -- Propulsion -- Structures and Loads -- Weights -- Stability, Control, and Handling Qualities -- Performance and Flight Mechanics -- Cost Analysis -- Sizing and Trade Studies -- Design of Unique Aircraft Concepts -- Conceptual Design Examples -- Appendix A: Unit Conversion -- Appendix B: Standard Atmosphere.
Holdings
Item type Current library Call number Copy number Status Date due Barcode
General Lending Carlow Campus Library General Lending 629.1341 (Browse shelf(Opens below)) 1 Available 58127
General Lending Carlow Campus Library General Lending 629.1341 (Browse shelf(Opens below)) 1 Checked out 24/01/2020 58013

Formerly CIP. Uk

Previous ed.: 1999.

Includes bibliographical references and index.

Design - A Separate Discipline -- Overview of the Design Process -- Sizing from a Conceptual Sketch -- Airfoil and Geometry Selection -- Thrust-to-Weight Ratio and Wing Loading -- Initial Sizing -- Configuration Layout and Loft -- Special Considerations in Configuration Layout -- Crew Station, Passengers, and Payload -- Propulsion and Fuel System Integration -- Landing Gear and Subsystems -- Intermission: Step-by-Step Development of a New Design -- Aerodynamics -- Propulsion -- Structures and Loads -- Weights -- Stability, Control, and Handling Qualities -- Performance and Flight Mechanics -- Cost Analysis -- Sizing and Trade Studies -- Design of Unique Aircraft Concepts -- Conceptual Design Examples -- Appendix A: Unit Conversion -- Appendix B: Standard Atmosphere.

125.89

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