Validation of a flexible aircraft take-off and landing analysis (FATOLA)
Huey D. Carden, John R. McGehee, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
National Aeronautics and Space Administration, Scientific and Technical Information Office, 1977 - Airplanes - 50 pages
What people are saying - Write a review
We haven't found any reviews in the usual places.
115K octal words 6600 series digital aerodynamic aileron deflection airframe flexibility analytical and flight analytical results analytical strokes angle of attack antisymmetric approximately axial strut forces central processing unit cockpit Computer Program Control Data 6600 control response Data 6600 series data accelerations elevator deflections elevons experimental and analytical FATOLA program Flexible Aircraft Take-off flexible-body option flight data flight test data friction force ft/sec g units gear axial strut gear strut stroke ground speed impact and rollout indicate Landing Analysis FATOLA Langley Research Center left gear left main gear left main gear-body NASA normal acceleration nose gear axial nose gear impact Nose gear touchdown option of FATOLA pitch attitude presented in figure refs right main rigid-body option roll autopilot roll rate series digital computer structural damping subroutine symmetric touchdown take-off and landing test and analytical test time histories tical U.S. Air Force variations YF-12A airplane YF-12A research airplane