Numerical and experimental study of the International Space Station crew quarters ventilation
The current paper proposes a detailed study of the ventilation system of the crew quarters
(CQ) aboard the International Space Station (ISS) in order to identify the ventilation system's …
(CQ) aboard the International Space Station (ISS) in order to identify the ventilation system's …
Study of Mesh Independence on The Computational Model of The Roll-up Vortex Phenomenon on Fighter and Delta Wing Models
ABSTRACT A good visualization technique is needed to analyze the flow around the aircraft
to see how much innovation can be made to improve the performance of a fighter. The use …
to see how much innovation can be made to improve the performance of a fighter. The use …
An evaluation of turbulence model for vortex breakdown detection over delta wing
An important phenomenon of delta wing is the mechanism of vortex core, which indicates
the increase in lifting force until the occurrence of the vortex breakdown. The computational …
the increase in lifting force until the occurrence of the vortex breakdown. The computational …
The influence of canard position on aerodynamic characteristics of aircraft in delaying stall conditions
The improvement of the performance of fighter aircraft is always made by doing engineering
flow around the fuselage; one way is by the addition of canard. The addition of a canard with …
flow around the fuselage; one way is by the addition of canard. The addition of a canard with …
Flow control with multi-dbd plasma actuator on a delta wing
MD Kesuma, R Irwansyah, J Julian, A Satyadharma - 2020 - catalog.lib.kyushu-u.ac.jp
In this study, an experiment was carried out to measure the performance of a delta wing with
65o swept angle. The measurement of lift and drag on the delta wing with and without …
65o swept angle. The measurement of lift and drag on the delta wing with and without …
Water tunnel flow visualization due to canard deflection effect on aircraft to improve stall delay performance
One of the advantages of the fighter is the ability to perform maneuver movements.
Modification of flow along the fuselage becomes very important in creating the ability to …
Modification of flow along the fuselage becomes very important in creating the ability to …
[HTML][HTML] Vortex dynamics analysis of straight-body-type-fuselage fighter using CFD simulation
The choice for using a fighter fuselage in a fighter jet design affects a vortex generation
advantageous in maneuverability. To study the effect of straight-body-type-fuselage (SBTF) …
advantageous in maneuverability. To study the effect of straight-body-type-fuselage (SBTF) …
Vortex dynamics study and flow visualization on aircraft model with different canard configurations
Canard configuration on fighter planes is essential for regulating flow and the occurrence of
vortex interactions on the main wing, one of which is to delay stall. Stall delays are useful …
vortex interactions on the main wing, one of which is to delay stall. Stall delays are useful …
Comparison of aerodynamic characteristics on Sukhoi SU-33-like and F-35 lightning II-like models using water tunnel flow visualization technique
Various fighter aircraft models have been developed following the design philosophy that
has been determined by the manufacturer. The development of fighter aircraft from various …
has been determined by the manufacturer. The development of fighter aircraft from various …
[PDF][PDF] Sutrisno
Canard configuration on fighter planes is essential for regulating flow and the occurrence of
vortex interactions on the main wing, one of which is to delay stall. Stall delays are useful …
vortex interactions on the main wing, one of which is to delay stall. Stall delays are useful …