Development of spin resistance criteria for light general aviation airplanes
Daniel J. DiCarlo, H. Paul Stough, Kelsey G Glover, P. BROWN, James M. Patton
Abstract
Daniel J. DiCarlo, H. Paul Stough, Kelsey G Glover, P. BROWN, James M. Patton
Abstract
A brief history of stall/spin technology for light general aviation airplanes is presented. Criteria needed to describe desirable characteristics of a spin-resistant airplane and means to evaluate airplanes for compliance with the criteria have been developed. Initial results from limited flight tests of an experimental high-wing airplane indicated that the basic configuration would not meet the spin resistance criteria. Further tests with the airplane modified to enhance its spin resistance are planned.
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A brief history of stall/spin technology for light general aviation airplanes is presented. Criteria needed to describe desirable characteristics of a spin-resistant airplane and means to evaluate airplanes for compliance with the criteria have been developed. Initial results from limited flight tests of an experimental high-wing airplane indicated that the basic configuration would not meet the spin resistance criteria. Further tests with the airplane modified to enhance its spin resistance are planned.
Key concepts: Aeronautics, Aviation, Aerospace engineering, Computer science, Spin (aerodynamics), Resistance (ecology), Engineering, Biology