Study on the Rudder Effect to the Lateral and Directional Flight Behaviors of the Turbojet Driven Light Aircraft

Ahmad Eshtiwey Al Aian; Bambang Basuno; Zamri bin Omar

doi:10.4028/www.scientific.net/AMM.660.481

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 660Study on the Rudder Effect to the Lateral and...

Study on the Rudder Effect to the Lateral and Directional Flight Behaviors of the Turbojet Driven Light Aircraft

Abstract:

The present work focuses on the development of computer code related to the lateral stability analysis on a jet engine aircraft model. The computer code designed in such a way, so for a given aircraft data will produce the result in term of: 1) Lateral directional dimensional stability derivatives, 2) Lateral directional responses following rudder maneuver with respect to the time, 3) The lateral direction transfer function for the rudder maneuvers, 4) The relationship between rudder deflection and lateral angle of attack (sideslip angle) β, the Euler roll angle ɸ, and Euler yaw angle ψ with respect to the time maneuvers. Through this developed computer code can make an assessment the lateral behavior for the turbojet driven light aircraft [1].

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Periodical:

Applied Mechanics and Materials (Volume 660)

Pages:

481-486

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.660.481

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Online since:

October 2014

Authors:

Ahmad Eshtiwey Al Aian, Bambang Basuno, Zamri bin Omar

Keywords:

Governing Equation of Flight Motion, Lateral, Lerajet-24, Transfer Function

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References

[1] Frederick O. Smetana, Flight Vehicle Performance and Aerodynamic Control, AIAA Education Series, Reston, Virginia, (2001).

Google Scholar

[2] Marcello Napolitano, Aircraft Dynamics: From Modeling to Simulation, (2012).

Google Scholar

[3] Frederick. O. Smetana, Delbert C. Summey, W. Donald Johnson: Riding and Handling Qualities of Light Aircraft: Review and Analysis, NASA CR – 1975, (1972).

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[4] Wayne Durham, Aircraft Flight Dynamics and Control, John Wiley & Sons, (2013).

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[5] Jan Roskam, Airplane Flight Dynamics and Automatic Flight Controls, Part 1, DAR Corporation, (2003).

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