Common aspects and differences in the behaviour of classical configuration versus canard configuration aircraft in the presence of vertical gusts, assuming the hypothesis of an elastic fuselage

Journal Title: INCAS BULLETIN - Year 2011, Vol 3, Issue 2

Abstract

The paper analyzes, in parallel, common aspects and differences in the behavior of classical configuration versus canard configuration aircraft in the presence of vertical gusts, assuming the hypothesis of an elastic fuselage. The effects of the main constructional dimensions of the horizontal empennage on lift cancelling and horizontal empennage control are being analyzed.

Authors and Affiliations

Octavian PREOTU, Alexandru DUMITRACHE, Mihai Aureliu LUNGU

Keywords

Related Articles

A review of some basic aspects related to integration of airplane’s equations of motion

Numerical integration of the airplane’s equations of motion has long been considered among the most fundamental calculations in airplane’s analysis. Numerical algorithms have been implemented and experimentally validated...

Aerodynamic Interference between Oscillating Lifting Surfaces and Fuselage Part 5: A Panel Method for Non-Lifting Bodies

In the fifth article of our series we will deal with the calculation of the unsteady aerodynamic forces on non-lifting bodies. We present here a contribution to the problem of the flow about non-lifting bodies. It is a p...

Attitude Dynamics of a Spinning Rocket with Internal Fluid Whirling Motion

This paper evaluates the impact that helical motion of fluid products of combustion within the combustion chamber of a rocket can have on the attitude dynamics of rocket systems. By developing the study presented by Sook...

Helicopter Roll-Axis Instabilities induced by Pilot Cyclic Control: A Physical Explanation

The main objective of this paper is to give a basic understanding of the mechanisms through which pilot cyclic inputs in lateral cyclic interacts with high-order rotor dynamics destabilizing the helicopter roll motion. T...

Investigation and design of a C-Wing passenger aircraft

A novel nonplanar wing concept called C-Wing is studied and implemented on a commercial aircraft to reduce induced drag which has a significant effect on fuel consumption. A preliminary sizing method which employs an opt...

Download PDF file
  • EP ID EP124364
  • DOI 10.13111/2066-8201.2011.3.2.7
  • Views 99
  • Downloads 0

How To Cite

Octavian PREOTU, Alexandru DUMITRACHE, Mihai Aureliu LUNGU (2011). Common aspects and differences in the behaviour of classical configuration versus canard configuration aircraft in the presence of vertical gusts, assuming the hypothesis of an elastic fuselage. INCAS BULLETIN, 3(2), 65-75. https://europub.co.uk./articles/-A-124364