Results 11 to 20 of about 10,032 (211)
International Journal of Aerospace Engineering, 2022 Hemisphere-on-cylinder turrets are the main airborne optical platform structure. However, an unsteady shock boundary layer interaction (SBLI) would act on flow separation and turbulent wake, which causes serious aero-optical effects with high spatial and
Xiang Ren +4 more
doaj +2 more sources
Integrated Numerical Simulation Research of High-speed Section in Transonic Wind Tunnel
Hangkong gongcheng jinzhan, 2020 For civil aviation aircraft with high subsonic economic cruising and fighter with high maneuverability at transonic speed, their demand for high-performance transonic wind tunnels is becoming more and more urgent, and integrated numerical simulation ...
YANG Xiaochuan +5 more
doaj +1 more source
Numerical and Experimental Analysis of Subsonic and Transonic Base Pressure
Journal of Physics: Conference Series, 2021 Base drag of space vehicles with large, truncated base usually forms a considerable component of overall drag. The base drag is usually difficult to be accurately predicted due to the intrinsic complexity of base flow.
Xiaobing Wang +5 more
semanticscholar +1 more source
A New Segmented Suction Slot Design Based on the Performance of Compressor Cascade
International Journal of Aerospace Engineering, Volume 2023, Issue 1, 2023., 2023 To develop an effective suction slot arrangement, computational fluid dynamics simulation software and a high subsonic compressor cascade were used to simulate different suction slots. Based on the effects of various suction slots on the cascade performance under various operating conditions, a novel segmented suction slot structure Seg3 was proposed ...
Fengming Li +5 more
wiley +1 more source
Numerical Simulations of Vertical Discrete Gusts Driven by Trailing Edge Blowing
International Journal of Aerospace Engineering, Volume 2023, Issue 1, 2023., 2023 A new type of gust generator generates the airflow oscillation in the wind tunnel through the Coanda effect of the unsteady trailing edge blowing, which has been shown to have strong potential for accurately simulating discrete gusts. It is necessary to study the relationship between the generated gust characteristics and the control parameters of such
Yang Shi +6 more
wiley +1 more source
Research on Wind Tunnel Test of Aerodynamic Characteristics of Missile under Subtransonic Velocity
Hangkong gongcheng jinzhan, 2020 In the process of missile design, the aerodynamic characteristics of missile as an important factor directly affect the dynamic quality of missile flight. In the case of severe nonlinearity of aerodynamic characteristics in subsonic and transonic regions,
PENG Bo, CEN Mengxi
doaj +1 more source
International Journal of Aerospace Engineering, Volume 2023, Issue 1, 2023., 2023 To examine the impact of oxidative jets on the thrust vector angle, secondary combustion efficiency, and combustion chamber pressure, inert gas (nitrogen) and pure oxygen are injected into the primary flow, which includes combustible components, at various locations in the divergence section and throat using different injection techniques.
Dongfeng Yan +5 more
wiley +1 more source
Investigation of Aeroelasticity Effect on Missile Separation from the Internal Bay
International Journal of Aerospace Engineering, Volume 2023, Issue 1, 2023., 2023 There is a strong aerodynamic interference when launching the missile in the embedded mode. During the separation process, the carrier aircraft safety may be threatened due to large slenderness ratio, low structural stiffness, and aeroelasticity effects of the missile. The present study simulates missile separation in the presence of the aeroelasticity
Shuling Tian +3 more
wiley +1 more source
Advances in Materials Science and Engineering, Volume 2022, Issue 1, 2022., 2022 In the era of fast transport, to create inventive stream flow management solutions that are capable of diminishing the aerodynamic drag of the vehicles, there is a need to modify the flow characteristics over the vehicle by deferring or expelling the position of the flow partition.
R. Srinath +5 more
wiley +1 more source
Flow visualization techniques, new developments and modernization of the existing Schlieren system in the Trisonic Wind Tunnel [PDF]
INCAS Bulletin, 2011 Schlieren flow visualization methods are an important part of high speed wind tunnel testing, being a fast and reliable method of graphically presenting complex dynamic phenomena that occur in high subsonic, transonic and supersonic regimes.
Marius PANAIT
doaj +1 more source