Arun Kumar et al., 2015 - Google Patents
Experimental study of subsonic and sonic jets controlled by air tabsArun Kumar et al., 2015
View PDF- Document ID
- 16447617706888360419
- Author
- Arun Kumar P
- Verma S
- Rathakrishnan E
- Publication year
- Publication venue
- Journal of Propulsion and power
External Links
Snippet
Tj= temperature of the jet at the nozzle exit Uc= jet velocity of the control jet Uj= primary jet velocity x= axial distance along the x axis y= distance along the Y axis (normal to the air tabs) z= distance along the Z axis (along the air tabs) μj= dynamic viscosity of the jet at the …
- 238000002156 mixing 0 description 49
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Arun Kumar et al. | Experimental study of subsonic and sonic jets controlled by air tabs | |
Kumar et al. | Truncated triangular tabs for supersonic-jet control | |
Kumar et al. | Fluidic injectors for supersonic jet control | |
Lubarsky et al. | Spray in crossflow: Dependence on Weber number | |
Quadros et al. | Study of effect of flow parameters on base pressure in a suddenly expanded duct at supersonic mach number regimes using CFD and design of experiments | |
Chauhan et al. | Mixing characteristics of underexpanded elliptic sonic jets from orifice and nozzle | |
Chutkey et al. | Analysis of annular plug nozzle flowfield | |
Sikroria et al. | Experimental investigation of liquid jet breakup in a cross flow of a swirling air stream | |
Quinn et al. | Mean streamwise centerline velocity decay and entrainment in triangular and circular jets | |
Rao et al. | Effect of nozzle geometry on flowfield for high subsonic jets | |
Gahlot et al. | Numerical study of supersonic mixed compression air intake with an array of air jets | |
Perumal et al. | Design of fluidic injector for supersonic jet manipulation | |
Park et al. | Nonlinear simulation of free surfaces and atomization in pressure swirl atomizers | |
Kumar et al. | Characteristics of controlled Mach 2 elliptic jet | |
Fu et al. | Absolute and convective instability of a confined swirling annular liquid layer | |
Khan et al. | Parametric study and scaling of Mach 1.5 jet manipulation using steady fluidic injection | |
Akram et al. | Control of supersonic elliptic jet with ventilated tabs | |
Mejia et al. | Experimental Investigation of Flow Interaction Dynamics in Supersonic Retropropulsion | |
Caeti et al. | Jet noise reduction via fluidic injection | |
Flock et al. | Experimental and numerical performance analysis of a self-starting three-dimensional scramjet intake | |
Nasif et al. | Numerical assessment of miniaturized cold spray nozzle for additive manufacturing | |
Ganesan et al. | Air-tab orientation effect on underexpanded sonic rectangular jet mixing | |
Paciorri et al. | Base-pressure experimental investigation on a space launcher in subsonic regime | |
Bouhanguel et al. | CFD Design Study of a Pressure Probe for Centerline Static Pressure Measurement in Supersonic Ejectors | |
Guildenbecher et al. | Pressure-scaling of pressure-swirl atomizer cone angles |