“CA”- Angular Lift Coefficient Theory in Horizontal Plane Takeoff Using Liquid Fuels

Abstract

In addition to providing knowledge to be added to existing methodologies, this theory reveals for builders and operators of highpower plant aircrafts a simple secret to having an aeronautical design in terms of desirable “cost x benefit” (economicity relation), considering CA ranging from 1.33 to 6.89 originated from the vision of “energy per mass”. Up to now the calculation of power plant to be installed in an aircraft is done empirically, despite all aeronautical knowledge, technical and scientific resources available. Then, the explain for continuous need using wind tunnels and/or lift software support.