Method to evaluate takeoff distance for nose-gear light aircrafts 2006-01-2753
The process of takeoff distance estimation for nose-gear light aircrafts involves several parameters such as aircraft total weight, runway type, engine power, aircraft geometry, aircraft aerodynamic characteristics, among others. This work demonstrates a method to evaluate the takeoff distance through monitoring the force system acting on the aircraft during the takeoff run. The numerical approach considers discrete time steps. Details of the implementation and limitations of the method are presented. Through this procedure it is possible to easily vary the basic aircraft configuration, allowing fast analysis of many different configurations to select the best for a particular performance.
Citation: Coelho, T., Cateb, A., Vieira, B., Minette, R. et al., "Method to evaluate takeoff distance for nose-gear light aircrafts," SAE Technical Paper 2006-01-2753, 2006, https://doi.org/10.4271/2006-01-2753. Download Citation
Author(s):
Thiago Campos Gondim Martins Coelho, André Carvalho Cateb, Bernardo Augusto de Oliveira Vieira, Ricardo Soares Minette, Rodrigo Sorbilli Cardoso de Sousa, Carlos Alberto Cimini
Affiliated:
Center for Aeronautic Studies of the Federal University of Minas Gerais - CEA/UFMG
Pages: 8
Event:
2006 SAE Brasil Congress and Exhibit
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Business and general aviation aircraft
Aircraft
Entry, descent, and landing
Aerodynamics
Runways
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