A SIMPLE GRAPHICAL METHOD FOR EVALUATING THE EFFECT OF THRUST VECTOR TILT ON THE AIRCRAFT PERFORMANCE.
AIR FORCE INST OF TECH WRIGHT-PATTERSON AFB OH SCHOOL OF ENGINEERING
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The semi-graphical method presented in the report may be useful for the preliminary performance computation for an aircraft with the variable thrust axis tilt. Application to different flight problems is shown. Optimization of some flight parameters can be achieved by simple graphical construction. Author
- Numerical Mathematics