Aircraft Engineering and Aerospace Technology: Volume 79 Issue 2

Strapline:

An International Journal
Subjects:

Table of contents

Flight simulation and testing of the FanWing experimental aircraft

O. Ahad, J.M.R. Graham

This paper aims to create an accurate computer‐based flight simulation of the FanWing experimental aircraft. The model would then be used to record and document the aircraft's…

1410

Design and CFD analysis of centrifugal compressor for a microgasturbine

Reza Aghaei tog, A. Mesgharpoor Tousi, M. Soltani

This paper aims to show how a good compressor can be designed and modeled with CFD steady models and to explain reasons for discrepancies between experiment (1D design) and 3D CFD…

2298

A low‐thrust guidance law based on Lyapunov feedback control and hybrid genetic algorithm

Ren Yuan, Cui Pingyuan, Luan Enjie

This paper seeks to examine the development of the on‐board guidance law for multi‐revolutions orbit transfer spacecraft with low‐thrust propulsion systems.

Flight flutter testing and aeroelastic stability of aircraft

Altan Kayran

To provide a general review of the flight flutter test techniques utilized in aeroelastic stability flight testing of aircraft, and to highlight the key items involved in flight…

1816

Crack detection in noisy environment including raining conditions

Vassilios Kappatos, Evangelos Dermatas

In outside constructions (e.g. aircraft frames, bridges, tanks and ships) real‐life noises reduce significantly the capability of location and characterization of crack events…

Helicopter stability and control in the presence of windshear

Yuan Su, Yihua Cao, Kungang Yuan

This paper aims to present a theoretical method for analyzing the stability and control of a hingeless helicopter in the presence of windshear.

Formulation for flutter and vibration analysis of a hingeless helicopter blade in hover: Part I

Ozge Ozdemir Ozgumus, Metin O. Kaya

This study aims to derive the kinetic and the potential energy expressions of a rotating uniform hingeless rotor blade and the aerodynamic loads that act on the blade element in…

1317

The FDM solution of unsteady inverse problem for two‐dimensional oscillating airfoils

Ai‐ling Yang, Zheng Yao, Gao‐lian Liu

This paper seeks to develop an approach for the unsteady inverse problem of two‐dimensional oscillating airfoils based on the finite difference method (FDM) solution of the…

48
Cover of Aircraft Engineering and Aerospace Technology

ISSN:

0002-2667

Online date, start – end:

1929

Copyright Holder:

Emerald Publishing Limited

Open Access:

hybrid

Editor:

  • Prof Phil Webb