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Cost Benefits of Aerodynamic Data Generation Techniques for Aircraft Stability and Control Analysis using the J2 Universal Tool-Kit

Journal Article
2008-01-2254
ISSN: 1946-3855, e-ISSN: 1946-3901
Published August 19, 2008 by SAE International in United States
Cost Benefits of Aerodynamic Data Generation Techniques for Aircraft Stability and Control Analysis using the J2 Universal Tool-Kit
Sector:
Citation: Jeffery, J. and Docksey, P., "Cost Benefits of Aerodynamic Data Generation Techniques for Aircraft Stability and Control Analysis using the J2 Universal Tool-Kit," SAE Int. J. Aerosp. 1(1):636-656, 2009, https://doi.org/10.4271/2008-01-2254.
Language: English

References

  1. Matthews Clifford AERONAUTICAL ENGINEERS DATA BOOK Butterworth-Heinemann Ltd 2001
  2. Hepperle, Martin JAVAFOIL – ANALYSIS OF AIRFOILS http://www.mh-aerotools.de/airfoils/javafoil.htm
  3. Drela Mark XFOIL – SUBSONIC AIRFOIL DEVELOPMENT SYSTEM http://web.mit.edu/drela/Public/web/xfoil
  4. Roskam, Jan AIRCRAFT DYNAMICS, AIRPLANE FLIGHT DYNAMICS AND AUTOMATIC FLIGHT CONTROL SYSTEMS Roskam Aviation and Engineering Corporation 1982
  5. Russell J B PERFORMANCE & STABILITY OF AIRCRAFT Edward Arnold 1996
  6. Panton Ronald L. INCOMPRESSIBLE FLOW Wiley-Interscience 1996
  7. Katz Joseph Plotkin Allen LOW-SPEED AERODYNAMICS: FROM WING THEORY TO PANEL METHODS McGraw-Hill Companies 1991
  8. Gibson JC THE DEFINITION, UNDERSTANDING AND DESIGN OF AIRCRAFT HANDLING QUALITIES Delft University of Technology 1995

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