ESTABLISHMENT OF CONTROL AND STABILITY MARGINS OF A PISTON ENGINE TRAINER AIRCRAFT

Authors

  • M.T. Ahmad M.T. Ahmad Aerospace Engineering Department, Faculty of Engineering, University Putra Malaysia, 43400 UPM, Serdang, Selangor, Malaysia
  • M.R. Ajir M.R. Ajir Aerospace Engineering Department, Faculty of Engineering, University Putra Malaysia, 43400 UPM, Serdang, Selangor, Malaysia
  • R. Varatharajoo R. Varatharajoo Aerospace Engineering Department, Faculty of Engineering, University Putra Malaysia, 43400 UPM, Serdang, Selangor, Malaysia

Keywords:

Stability, Static Stability, Stick Fixed and Stick Free Neutral Point, Flight Test

Abstract

A programme was initiated to investigate the control and stability margin of the MD3-l60
aircraft with a view to possibly expand the center of gravity envelope which is currently
restrictive. Non-standard modifications were carried out to install the instruments to measure
elevator position. trim lab position, stick-forces and greading. Flight test were carried on
aircraft S/N 008 which belongs to the Royal Malaysian Air Force. The test flights were conducted
to establish control and stability margins within the current center of gravity envelope.

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Published

2018-04-25

How to Cite

M.T. Ahmad, M. A., M.R. Ajir, M. A., & R. Varatharajoo, R. V. (2018). ESTABLISHMENT OF CONTROL AND STABILITY MARGINS OF A PISTON ENGINE TRAINER AIRCRAFT. Jurnal Mekanikal, 18(2). Retrieved from https://jurnalmekanikal.utm.my/index.php/jurnalmekanikal/article/view/206

Issue

Issue 18: December 2004

Section

Mechanical

License

Copyright of articles that appear in Jurnal Mekanikal belongs exclusively to Penerbit Universiti Teknologi Malaysia (Penerbit UTM Press). This copyright covers the rights to reproduce the article, including reprints, electronic reproductions or any other reproductions of similar nature.

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