www.Airloads.net

The results which we reach by practical flying experiments will depend most of all upon the shapes which we give to the wings used in experimenting — Otto Lilienthal, 1896

Comparing Aerodynamic Results With

• NACA - Experimental Wind-Tunnel Tests
• AeroFoil - Donald L.Reid - Virginia State University - USA
• DesignFoil - John Dreese - Ohio State University - USA
• JavaFoil - Dr. Martin Hepperle - Braunschweig - Germany
• Kevin's Code - Dr. Kevin D.Jones - Naval Postgraduate School - USA
• Pablo - Christian Wauquiez - Royal Institute of Technology - Sweden
• XFOIL - Prof. Mark Drela & Harold Youngren - Massachusetts Institute of Technology - USA
• AVL - Prof. Mark Drela & Harold Youngren - Massachusetts Institute of Technology - USA
• LinAir - Dr. Ilan Kroo At Stanford University And Developed By Donald A.Durston At NASA Ames Research Center - Copyrights By Desktop Aeronautics,Inc - California - USA
• Monoplane Equation - Dr. James F.Marchman - Virginia Polytech Institute And State University - USA
• Multisurface Aerodynamic - Dr. Patrick Hanley - Hanley Innovations - USA
• Surfaces - Great Owl Publishing Engineering Software
• Tornado - A Cooperation Between The Royal Institute of Technology (KTH) , University of Bristol , Linköping University And Redhammer Consulting Ldt. - Sweden
• USAF Datcom - The United States AirForce Stability And Control Data Compendium - Copy Made By Public Domain Aeronautical Software (PDAS) - California - USA
• VLAERO - AMI Analytical Methods Inc. - USA
• XFLR5 - Andre Deperrois

Test Cases (Old Versions)

• 1 – Infinite Flat Plate
• 2 – Circular & Elliptical 2D Surfaces
• 3 – Karman–Trefftz Airfoil
• 4 – NACA TR 824 – 0015 Symmetric
• 5 – NACA TR 824 – 2412 Four Series
• 6 – NACA TR 537 – 23012 Five Series Airfoil
• 7 – NACA TR 537 – 23012 Reflexed Five Series Airfoil
• 8 – NACA TR 537 –25012 Reflexed Five Series Airfoil
• 9 – NACA TR 537 –Wing Number Three
• 10 – NACA TR 537 – Wing Number Seven
• 11 – NACA TR 537 – Wing Number Nine
• 12 – NACA TN 1269 – Wing Number One
• 13 – NACA TN 1269 – Wing Number Two
• 14 – NACA TN 1269 – Wing Number Three
• 15 – NACA TN 1422 – Wing Number One
• 16 – NACA TN 1422 – Wing Number Two
• 17 – NACA TN 1422 – Wing Number Three
• 18 – Random Wing (AR = 6)
• 19 – Flat Plate Wing (AR = 10)
• 20 – Flat Plate Wing (AR = 2.352)
• 21 – Complete Aircraft Configurations
• 22 – Supersonic Missile (Mach 4)
• 23 – Sharp Delta Wing (Mach 6)
• 24 – XB-70 (Mach 2.4)
• 25 – XB-70 (Mach 4)
• 26 – Arrow Wing (Mach 4)
• 27 – Arrow Wing (Mach 3)
• 28 – Swept Cambered Wing (Mach 3)
• 29 – Sukhoi-37 (Mach 2.5)
• 30 – AIM-7 Missile (Mach 4.6)
• 31 – Rectangular Wing (Mach 2)
• 32 – NASA TN-D-3767 - Leading Suction Analogy