Effect of Side Wind on the Directional Stability and Aerodynamics of a Hybrid Buoyant Aircraft

Directional stability characteristics explain the capabilities of a hybrid buoyant aircraft’s performance against the side wind, which induces flow separation that is chaotic in nature and may lead to oscillations of the aerodynamic surfaces. A numerical study is carried out to estimate the effect o...

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Main Authors: Haque Anwar U, Asrar Waqar, Omar Ashraf A, Sulaeman Erwin, Ali Mohamed J.S
Format: Article
Language:English
Published: EDP Sciences 2016-01-01
Series:MATEC Web of Conferences
Online Access:http://dx.doi.org/10.1051/matecconf/20164002006
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spelling doaj-0932ded62ab64823b4f4c188cfb7da852021-02-02T00:03:57ZengEDP SciencesMATEC Web of Conferences2261-236X2016-01-01400200610.1051/matecconf/20164002006matecconf_icmes2016_02006Effect of Side Wind on the Directional Stability and Aerodynamics of a Hybrid Buoyant AircraftHaque Anwar U0Asrar Waqar1Omar Ashraf A2Sulaeman Erwin3Ali Mohamed J.S4International Islamic University Malaysia (IIUM)International Islamic University Malaysia (IIUM)University of Tripoli (UOT)International Islamic University Malaysia (IIUM)International Islamic University Malaysia (IIUM)Directional stability characteristics explain the capabilities of a hybrid buoyant aircraft’s performance against the side wind, which induces flow separation that is chaotic in nature and may lead to oscillations of the aerodynamic surfaces. A numerical study is carried out to estimate the effect of side wind. The boundary conditions for the computational domain are set to velocity inlet and pressure outlet. Due to the incompressible flow at the cruise velocity, the density is taken to be constant. For these steady state simulations, the time is discretized in first order implicit and the SIMPLE scheme is employed for pressure velocity coupling alongwith k-ω SST model. Based on the results obtained so far, it is concluded that voluminous hybrid lifting fuselage is the major cause of directional.http://dx.doi.org/10.1051/matecconf/20164002006
collection DOAJ
language English
format Article
sources DOAJ
author Haque Anwar U
Asrar Waqar
Omar Ashraf A
Sulaeman Erwin
Ali Mohamed J.S
spellingShingle Haque Anwar U
Asrar Waqar
Omar Ashraf A
Sulaeman Erwin
Ali Mohamed J.S
Effect of Side Wind on the Directional Stability and Aerodynamics of a Hybrid Buoyant Aircraft
MATEC Web of Conferences
author_facet Haque Anwar U
Asrar Waqar
Omar Ashraf A
Sulaeman Erwin
Ali Mohamed J.S
author_sort Haque Anwar U
title Effect of Side Wind on the Directional Stability and Aerodynamics of a Hybrid Buoyant Aircraft
title_short Effect of Side Wind on the Directional Stability and Aerodynamics of a Hybrid Buoyant Aircraft
title_full Effect of Side Wind on the Directional Stability and Aerodynamics of a Hybrid Buoyant Aircraft
title_fullStr Effect of Side Wind on the Directional Stability and Aerodynamics of a Hybrid Buoyant Aircraft
title_full_unstemmed Effect of Side Wind on the Directional Stability and Aerodynamics of a Hybrid Buoyant Aircraft
title_sort effect of side wind on the directional stability and aerodynamics of a hybrid buoyant aircraft
publisher EDP Sciences
series MATEC Web of Conferences
issn 2261-236X
publishDate 2016-01-01
description Directional stability characteristics explain the capabilities of a hybrid buoyant aircraft’s performance against the side wind, which induces flow separation that is chaotic in nature and may lead to oscillations of the aerodynamic surfaces. A numerical study is carried out to estimate the effect of side wind. The boundary conditions for the computational domain are set to velocity inlet and pressure outlet. Due to the incompressible flow at the cruise velocity, the density is taken to be constant. For these steady state simulations, the time is discretized in first order implicit and the SIMPLE scheme is employed for pressure velocity coupling alongwith k-ω SST model. Based on the results obtained so far, it is concluded that voluminous hybrid lifting fuselage is the major cause of directional.
url http://dx.doi.org/10.1051/matecconf/20164002006
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