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Supporting system interference on aerodynamic characteristics of an aircraft model in a low-speed wind tunnel
Abstract Many kinds of support system, such as tail support system, external/balance support system, side wall support system and wing tip support system are used for wind tunnel testing. TheExpand
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Contemporary frame of measurement and assessment of wind-tunnel flow quality in a low-speed facility
The requirements for the accuracy of measurements in a wind tunnel test become more and more severe while the complexity of the test increases. In an environment of reduced time available for windExpand
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Experimental and numerical study of super-critical flow around the rough sphere
This paper presents the experimental and numerical research on the sphere model with the goal of prediction of a flow behaviour in a presence of the surface roughness. Results indicate the problemsExpand
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Experimental and numerical research of the influence of thrust vector control on the missile aerodynamics by cold and hot jet simulations
The flow field phenomena that occur as a result of thrust vector control (TVC) system activity on a missile with lateral jets are very complex and influence all other components of the missile.Expand
AERODYNAMIC SHAPE OPTIMIZATION OF GUIDED MISSILE BASED ON WIND TUNNEL TESTING AND CFD SIMULATION by
TLDR
This paper presents modification of the existing guided missile which was done by replacing the existing front part with the new five, while the rear part of the missile with rocket motor and missile thrust vector control system remains the same. Expand
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Aerodynamic shape optimization of guided missile based on wind tunnel testing and computational fluid dynamics simulation
This paper presents modification of the existing guided missile which was done by replacing the existing front part with the new five, while the rear part of the missile with rocket motor and missileExpand
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Observations on some transonic wind tunnel test results of a standard model with a T-tail
As a part of a periodic health monitoring of the wind tunnel structure, instrumentation and flow quality, a series of tests of an AGARD-C calibration model was performed in the 1.5 m T-38 trisonicExpand
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Aerodynamic interceptors efficiency for subsonic missiles roll attitude control
TLDR
The excessive roll of air-launched missiles is a result of disturbances during the flight due to airframe misalignment, asymmetric control in pitch and yaw planes, atmospheric disturbances or large torque disturbances. Expand
Aerodynamic testing model guided missiles with jets simulations in the T-35 wind tunnel
Testing of the Anti-Tank Missile with jets simulations in the T-35 wind tunnel is part of the development program of short range anti-tank system. The main task of this experiment was to provide anExpand