Zobrazeno 1 - 10
of 44
pro vyhledávání: '"K., Vijayaraja"'
Publikováno v:
Aircraft Engineering and Aerospace Technology, 2021, Vol. 93, Issue 7, pp. 1193-1203.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/AEAT-10-2020-0225
Autor:
Manigandan, S., K., Vijayaraja
Publikováno v:
Aircraft Engineering and Aerospace Technology, 2018, Vol. 90, Issue 9, pp. 1364-1371.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/AEAT-04-2017-0111
Publikováno v:
Aircraft Engineering and Aerospace Technology. 93:1193-1203
Purpose The effect of increasing lip thickness (LT) and Mach number on subsonic co-flowing Jet (CFJ) decay at subsonic and correctly expanded sonic Mach numbers has been analysed experimentally and numerically in this study. This study aims to a crit
Publikováno v:
International Journal of Vehicle Structures and Systems. 13
The experimental setup of applied-field Magneto Plasma Dynamic Thruster (MPDT) is a form of electrically powered spacecraft propulsion system. The thrusters are used for deep space mission, which consist of long duration, low thrust acceleration and
Autor:
A. Anderson, S. Manigandan, Sriram Venkatesh, P. Gunasekar, K. Vijayaraja, R. Gokulnath, Rakesh Vimal
Publikováno v:
International Journal of Ambient Energy. 43:918-923
Aerodynamic force plays a major role in motorsport since it is independent of the forced system. The efficient aerodynamic car has the capability of consuming less energy and better vehicle handlin...
Publikováno v:
International Journal of Vehicle Structures and Systems. 13
Base drag, arising from flow separation at the blunt base of a body can be a sizeable fraction of total drag in the context of projectiles, missiles and after bodies of fighter aircrafts. The base drag is the major contribution of total drag for low
Autor:
S. Manigandan, K. Vijayaraja
Publikováno v:
Aircraft Engineering and Aerospace Technology. 90:1364-1371
Purpose The purpose of this paper is to present the results of mixing promotion and screech frequency of controlled elliptical supersonic jet. Design/methodology/approach Flow field characteristics of low-aspect-ratio elliptical jets are examined at
Autor:
K. Vijayaraja, S. Manigandan
Publikováno v:
International Journal of Turbo & Jet-Engines. 38:193-201
The acoustic and flow characteristics of a jet with elliptical throat is studied at different levels of nozzle expansion ratio. In this study, we have taken two types of CD nozzle configuration (circular and elliptical throat) and it is studied for v
Autor:
S. Manigandan, K. Vijayaraja
Publikováno v:
International Journal of Ambient Energy. 40:854-857
In this paper, we study the energy decay characteristics of the nozzle at supersonic velocity. We have taken three types of configuration: circular, square and elliptical. The results are compared ...
Autor:
S. Manigandan, K. Vijayaraja
Publikováno v:
International Journal of Ambient Energy. 40:57-62
The mixing characteristic of circular jet with elliptical throat is studied at different levels of expansion of the nozzle. Two kinds of configurations are studied in this paper, elliptical throat ...