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2261
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2262
Characterization and mitigation of blade waviness effects on fan performance
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Thesis -
2263
Methods of Aircraft Charge Control During Flight
Published 2022“…The system demonstrates comparable results to previous modeling and wind tunnel experiments, which showed an increase in plane potential and a decrease in corona current as wind speed increased. …”
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Thesis -
2264
An Experimental Investigation of Blown-Flap Airfoils
Published 2022“…A quasi 2-dimensional wind tunnel model is used to conduct surveys on both the performance and flow characteristics of propeller blown-flap airfoils. …”
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Thesis -
2265
Design and development of a high-altitude, in-flight-deployable micro-UAV
Published 2013Get full text
Thesis -
2266
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2267
Analysis of civil aircraft propulsors with boundary layer ingestion
Published 2015Get full text
Thesis -
2268
Development of longitudinal flight simulator
Published 2022“…The core simulation engine is built in Simulink and the input are attitudes of the aircraft model in wind tunnel and the forces experienced by the aircraft model in inertial frame of reference. …”
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Final Year Project (FYP) -
2269
Investigating Galilean invariance in CFD
Published 2023“…When characterizing a body moving in a quiescent flow, like the case of a cruising aircraft, CFD simulations and wind tunnel tests rely on the Galilean invariance principle, which assumes that the moving body can be equivalently modelled by a stationary body with a freestream velocity equal to the motion velocity of the body. …”
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Thesis-Master by Research -
2270
Measurements of a heated low speed channel
Published 2010“…The low air velocity inside the wind tunnel of the test rig will be controlled and kept constant by a pulse width modulation circuit. …”
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Final Year Project (FYP) -
2271
Computational modeling of the aerodynamic characteristics and flight mechanics and control of an unmanned aerial vehicle
Published 2010“…By combining these estimates with wind tunnel data, a comprehensive aerodynamic characteristics model is constructed for augmenting the flight dynamics model of the UAV. …”
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Thesis -
2272
A simplified gas flow meter
Published 2011“…The skid set-up comprises of a wind tunnel, filter, slam shut valve and turbine gas meter with the rationale of simulating the actual working conditions of a distribution network regulating station of Town Gas. …”
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Final Year Project (FYP) -
2273
Design and development of joined-wing aircraft
Published 2015“…Testing was done using both CFD simulations, and wind tunnel testing on actual models, focusing on the lift and drag coefficients. …”
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Final Year Project (FYP) -
2274
Actuation and control of wing warping via tendon-sheath mechanism for flexible membrane wing mini-UAV
Published 2018“…Further verifications such as computational fluid dynamic simulations, wind tunnel tests and flight tests were conducted to show the robustness and real world usability of the TSM wing warping controller on the FMW mini-UAV. …”
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Thesis -
2275
Aerodynamics of badminton shuttlecock : Characterization of flow around a conical skirt with gaps, behind a hemispherical dome
Published 2014“…Some of the numerical results were validated against wind tunnel experiments. The numerical and experimental results showed good agreement.…”
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Journal Article -
2276
Tendon-sheath mechanisms in flexible membrane wing mini-UAVs : control and performance
Published 2018“…The proposed approach is validated experimentally in a wind tunnel facility with imitated gusty condition and subsequently tested in a real flight condition. …”
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Journal Article -
2277
Studi Eksperimental Perpindahan Kalor dan Penurunan Tekanan Aliran Udara Melintasi Penukar Kalor Kompak Tabung Eliptik Susunan Berseling
Published 2014“…Experiments are conducted in the subsonic wind tunnel with air velocity of 1 m/s to 12 m/s under uniform heat fluxes of 3.7 kW/m2, 3.8 kW/m2 and 3.9 kW/m2. …”
Thesis -
2278
Effects of canard configuration on the aerodynamics of blended wing body at low mach number / Zurriati Mohd Ali
Published 2015“…The experimental works were performed on a scale model and tested in a low speed wind tunnel. Angles of attack, a varied from -10 to 10 degree, as well as canard setting angles, 8. …”
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Thesis -
2279
Longitudinal flight dynamics and stability of blended wing-body unmanned aerial vehicle with canard as control surface / Rizal Effendy Mohd Nasir
Published 2014“…This study proposes simple scheduled feedback gains to the canard. Wind tunnel experiments, computational simulations and empirical estimations were conducted to characterize its aerodynamics and to come up with its aerodynamic mathematical model for flight dynamics derivatives calculation. …”
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Book Section -
2280
Heat transfer in the core compressor under ice crystal icing conditions
Published 2018“…The plate was installed in the Altitude Icing Wind Tunnel (AIWT) at the National Research Council of Canada (NRC). …”
Journal article