Spin Resistance Evaluation of a Light Airplane
H. Paul Stough, Daniel J. DeCarlo, James M. Patton
Abstract
H. Paul Stough, Daniel J. DeCarlo, James M. Patton
Abstract
A brief history of stall/spin technology for light general aviation airplanes and proposed criteria to describe desirable characteristics of a spin-resistant airplane are presented. Flight tests of a representative light airplane to evaluate compliance with and usefulness of the criteria are presented. The baseline airplane configuration would not meet the spin resistance criteria. Tests of the airplane with a wing leading edge modification to enhance its spin resistance showed compliance with the proposed criteria.
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A brief history of stall/spin technology for light general aviation airplanes and proposed criteria to describe desirable characteristics of a spin-resistant airplane are presented. Flight tests of a representative light airplane to evaluate compliance with and usefulness of the criteria are presented. The baseline airplane configuration would not meet the spin resistance criteria. Tests of the airplane with a wing leading edge modification to enhance its spin resistance showed compliance with the proposed criteria.
Key concepts: Airplane, Spin (aerodynamics), Resistance (ecology), Computer science, Aerospace engineering, Engineering, Biology, Ecology