TAIL PLANE DESIGN FOR SATISFYING LONGITUDINAL HANDLING QUALITIES | ||
| Anbar Journal of Engineering Sciences | ||
| Editorial, Volume 1, Issue 2, November 2008, Pages 1-14 PDF (254.13 K) | ||
| DOI: 10.37649/aengs.2008.14201 | ||
| Authors | ||
| Yahya A. Faraj; Farag M. Mohammed; Mohammed A. Ahmed; Mohammed A. Ahmed; Waleed M. Abid; Ahmed N. Uwayed; Ghalib R. Ibrahim; Khaldon F. Breithe; Khalel I. Aziz; Arz Y. R; Hamdi E. A. Zangana; Akram Shaker Mahmood; Arz Yahya Rzayeg; Ahmed T. Al; ; Khaleel I. Aziz; Mazin Y.A; Riyah N. K; Nidaa Ezzy; Khamis N. Sayle; Nidaa Ezzy; xxxxx xxxxx; xxxxx xxxxxxx; xxxxx xxxxxx; zzzzzz zzzzzz | ||
| Abstract | ||
| The Cooper-Harper rating of aircraft handling qualities has been adopted as a standard for measuring the performance of aircraft. In the present work, the tail plane design for satisfying longitudinal handling qualities has been investigated with different tail design for two flight conditions based on the Shomber and Gertsen method. Tail plane design is considered as the tail/wing area ratio. Parameters most affecting on the aircraft stability derivative is the tail/wing area ratio. The longitudinal handling qualities criteria were introduced in the mathematical contributions of stability derivative. This design technique has been applied to the Paris Jet; MS 760 Morane-Sualnier aircraft. The results show that when the tail/wing area ratio increases the aircraft stability derivative increases, the damping ratio and the natural frequency increases and the aircraft stability is improved. Three regions of flight conditions had been presented which are satisfactory, acceptable and unacceptable. The optimum tail/wing area ratio satisfying the longitudinal handling qualities and stability is (0.025 Keywords Longitudinal Handling --- Stability --- Tail Design | ||
| Keywords | ||
| Longitudinal Handling; stability; Tail Design; Laminar Flow; mixed convection; Porous Medium; Tube banks; numerical study; heat transfer; Natural Convection; and Eccentricity; vibration; ANSYS; Crack; free; layer; continuous; Partial; Interaction; composite material; cutout; laminate; composite plate; Normal Strain; Tensile Load; Friction factor; Vortex Generator; Triangular Duct; Fully Developed Turbulent flow; Nonlinear Material; finite element; Epoxy; Polyester; Tension Softening; and Enhanced Multilinear Isotropic Softening; multi; composite; beam; Blast; simply supported; impact; hypervelocity; Penetration; jet; wax; Pollution; acoustic; Treatment; Environment; Threshold; Auditorium; performance; reverberation; intelligibility; Reflection | ||
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