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Introduction to Aeronautics 2nd ed.

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丛书名： AIAA Education Series

2004年

作者： Steven A. Brandt John J. Bertin Randall J. Stiles Ray Whitford

ISBN: (数字)9781600862007

ISBN: (纸本)9781563477010

The most exciting moment for an aeronautical engineer is when his or her design becomes a working aircraft, the endpoint of a journey that begins in the classroom. This textbook provides the resources that students need to understand the methods and thought processes involved in designing aircraft. Students learn through the use of specific analytical principles, practical examples, case studies, and corresponding problems to solve. The material in this textbook and AeroDYNAMIC 3.0 software (purchased separately) is sufficient to support a university-level course of three to six semester hours. At the U.S. Air Force Academy (USAFA), Chapters 1-6 are used in a three-semester-hour course taught to the entire student body. The material in Chapters 7-10 is taught at USAFA in later courses taken only by aeronautical engineering majors.For professors, this textbook comes complete with end-of-chapter homework problems that provide a summary of the concepts and features contained in the chapters. The problems provide students with an excellent opportunity to analyze and synthesize industry examples, ensuring they understand the key concepts and their applications. A Windows-based software package on DVD (purchased separately), entitled AeroDYNAMIC, provides a single integrated package with one universal user interface providing access to virtual laboratories, simulations, and design synthesis and analysis software based on the methods presented in the text.

关键词： Aircraft Components and Structure Aircraft Design Aircraft Operations and Technology Aircraft Stability and Control Aircraft wing Components Aircraft wing Design Aircrafts Airfoil Airfoil Nomenclature Flight Control Surfaces wing Configurations wing planforms

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Flight Vehicle Performance and Aerodynamic Control

引用

丛书名： AIAA Education Series

2001年

作者： Frederick O. Smetana

ISBN: (数字)9781600861857

ISBN: (纸本)9781563474637

Flight Vehicle Performance and Aerodynamic Control is designed to serve as a text for either an 11-week or a 16-week course at the sophomore level. It explains typical methods used to estimate aircraft performance, the theoretical basis of these methods, and how various parameters derived from the aircraft geometry can be used to estimate the requirements of control surfaces and the aerodynamic forces required to actuate these surfaces. This book includes time-tested computer programs that perform the analyses in a manner that reduces student error and improves result accuracy. Because the source code is given, users with a FORTRAN compiler can modify the program to suit particular needs. The major advantage of the software is that more realistic problems may be treated and the effects of parametric programs are more accurate than calculators. The programs are available as executables for Windows machines as well as in ASCII source code versions that can be readily compiled and then executed on Unix, Linux, and Macintosh machines, and on mainframes.

关键词： Aerodynamic Performance Aerodynamics Aeronautical Engineering Aeronautics Aerospace Engineering Aerospace Sciences Aircraft Carriers Aircraft Components and Structure Aircraft Conceptual Design Aircraft Design Aircraft Dynamic Modes Aircraft Engines Aircraft Instruments Aircraft Operations Aircraft Operations and Technology Aircraft Performance Aircraft Stability and Control Aircraft Stabilizer Aircraft wing Components Aircraft wing Design Aircrafts Airfoil Airfoil Nomenclature Airspeed Astrodynamics Astronautics Atmospheric Science Aviation Aviation Authorities and Organizations Aviation Safety Avionics Civil Aviation Combat Aircraft Combustion Chambers Compressors Energy Energy Conversion Energy Economics Energy Forms Energy Forms, Production and Conversion Energy Production Fixed-wing Aircraft Flight Control Surfaces Flight Dynamics Flight Mechanics Flight Test Flight Training Fluid Dynamics Fluid Flow Properties Fluid Mechanics Fossil Fuels Fuel Injection Fuels Gas Turbine Guidance, Navigation, and Control Systems Heat Engines Helicopters Hydraulics Hydrodynamics Ignition Systems Jet Aircraft Liquid Fuels Longitudinal Static Stability Military Airbases Military Aircraft Military Aviation Non-Renewable Energy Petroleum Power Station Propulsion and Power Reciprocating Engine Rocket Engine Rocketry Rotorcrafts Sensors Short Takeoff and Landing Takeoff and Landing Transducers Turbines Turbomachinery Unmanned Aerial Vehicle Wind Engineering Wind Tunnels Wind Turbine wing Configurations wing planforms

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