[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

Rajesh et al., 2018 - Google Patents

Effect of dimensions of various spikes of a spiked cylinder on the buzz phenomenon subjected to hypersonic flows

Rajesh et al., 2018

Document ID
12596364856357584919
Author
Rajesh R
Rakesh S
Publication year
Publication venue
International Journal of Fluid Mechanics Research

External Links

Snippet

Transient numerical analysis has been carried out by simulating the fluid flow over sharp, conical, blunt, hemispherical, and aerodisk spiked cylinders. They have been subjected to hypersonic flow of Mach number 6.1, at zero angle of attack, so as to investigate the …
Continue reading at www.dl.begellhouse.com (other versions)

Similar Documents

Publication Publication Date Title
Zhang et al. Mechanism of frequency lock-in in vortex-induced vibrations at low Reynolds numbers
Watanabe et al. Three-dimensional vortex structures under breaking waves
Azarova et al. Pulsating stochastic flows accompanying microwave filament/supersonic shock layer interaction
Le et al. On the structure of vortex rings from inclined nozzles
Venkatachari et al. Numerical investigation of the interaction of counterflowing jets and supersonic capsule flows
Smith et al. Turbulent wall-layer vortices
Zhang et al. The starting flow structures and evolution of a supersonic planar jet
Rajesh et al. Effect of dimensions of various spikes of a spiked cylinder on the buzz phenomenon subjected to hypersonic flows
Wu et al. Response of a turbulent separation bubble to zero-net-mass-flux jet perturbations
Zhu et al. The formation process of annular starting jets
Li et al. Experimental investigation of flow separation in a planar convergent-divergent nozzle
Ramachandran et al. Effect of dimensions of sharp spiked cylinder on the buzz phenomenon subjected to hypersonic flows
Luo et al. The dynamics of a bubble in the internal fluid flow of a pipeline
De et al. Evolution of wake structure with aspect ratio behind a thin pitching panel
Xie et al. Numerical investigation on spray characteristics with upstream flow pulsation of a pintle injector
Sahoo et al. Effect of body nose fairing on the unsteady flow characteristics over spiked flat faced cylinder at supersonic speed
Gao et al. Research on the cavitation flow interference and impact loads of successively launched underwater projectiles
Zou et al. On the stability of supercavity with angle of attack
Simonenko et al. On the supersonic flow over an axisymmetric step at an angle of attack
Pan et al. Numerical study of periodically forced-pitching of a supercavitating vehicle
Vashishtha et al. Novel mechanism of instability control using a tapered spike in hypersonic flow
Prakash et al. Effect of Mach number and turbulent characteristics of chevrons nozzles in high-speed aircraft jet-CFD analysis by aero acoustic phenomenon
Duvvuri et al. On shock-wave unsteadiness in separated flows
Uruba Flow control using synthetic jet actuators
Vashishtha et al. Mach number dependence of flow instability around a spiked body