First Page | Document Content | |
---|---|---|
![]() Date: 2006-05-16 18:09:39Fluid dynamics Micro air vehicle Angle of attack Stall Dihedral Fixed-wing aircraft Wing loading Lift coefficient Lift-to-drag ratio Aerospace engineering Aerodynamics Aviation | Source URL: www.mil.ufl.eduDownload Document from Source WebsiteFile Size: 781,71 KBShare Document on Facebook |
![]() | PO 18 THE SOUTH AFRICAN MODEL AIRCRAFT ASSOCIATION DEFINITION AND SPECIFICATION OF MODEL AIRCRAFT IssueIssueDocID: 1rmKe - View Document |
![]() | WHY ROTORS INSTEAD OF WINGS by Greg Gremminger When I first got into gyrocopters, I had been flying fixed-wing airplanes and ultralights for many years. What attracted me to gyrosDocID: 1qGgr - View Document |
![]() | 1 The South African Model Aircraft Association SAMAA Proficiency tests for fixed-wing powered modelsDocID: 1qBZU - View Document |
![]() | Aeronautics Educator Guide pdfDocID: 1qnjW - View Document |
![]() | AERIAL ISR - FIXED WING & ROTOR AIRCRAFT Aeronautics AERIAL ISR Aerial ISR (Intelligence, Surveillance and Reconnaissance) isDocID: 1qm4B - View Document |