Zobrazeno 1 - 10
of 22
pro vyhledávání: '"S. M., Aravindh Kumar"'
Autor:
GOVINDAN, Mahendra Perumal1,2 mahendrg@srmist.edu.in, S. M., Aravindh Kumar2, S., Elangovan1, M., Sundararaj1
Publikováno v:
Journal of Thermal Engineering. May2024, Vol. 10 Issue 3, p585-598. 14p.
Autor:
G. Kailash, S. M. Aravindh Kumar
Publikováno v:
Recent Advances in Applied Mechanics ISBN: 9789811695384
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::98bbdab7146fa7cdeaac6e7b43795336
https://doi.org/10.1007/978-981-16-9539-1_6
https://doi.org/10.1007/978-981-16-9539-1_6
Publikováno v:
International Review of Aerospace Engineering; Feb2023, Vol. 16 Issue 1, p1-8, 8p
Publikováno v:
Journal of Physics: Conference Series. 2054:012079
The sonic coflow effect on the core length of sonic primary jet was experimentally investigated in this research work. A circular convergent nozzle was used for both core and coflow jet studies. The 1mm annular gap was maintained between the coflow a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3125ca8eee98741c44cf71aab4e880b9
https://doi.org/10.1088/1742-6596/2054/1/012079
https://doi.org/10.1088/1742-6596/2054/1/012079
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 231:1460-1477
Elliptic jet mixing influenced by triangular tabs is demonstrated in this work. Mixing modification of a Mach 2 jet from a convergent-divergent elliptic nozzle of aspect ratio 2, in the presence of two triangular tabs along the major and minor axis a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c99ec1a6a069e27079e66d0c41978088
https://doi.org/10.1177/0954410016652921
https://doi.org/10.1177/0954410016652921
Publikováno v:
The Aeronautical Journal. 120:1197-1214
The effects of aspect ratio on elliptical sonic jet decay at different levels of under-expansion has been studied experimentally. Elliptical sonic jets from orifices of same area with aspect ratios (AR) 2, 4 and 6 at nozzle pressure ratios 2 to 5 in
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5d5651a0f1633a7a8ca517020acf1ae1
https://doi.org/10.1017/aer.2016.55
https://doi.org/10.1017/aer.2016.55
Publikováno v:
The Aeronautical Journal. 120:495-519
Comparative mixing of a Mach 2 elliptical free jet from a convergent-divergent elliptic nozzle with an aspect ratio of 2:1 in the presence of adverse and marginally favourable pressure gradients has been studied experimentally. It is found that the m
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3fed4f164f8b662164d6bd0cd85e2b76
https://doi.org/10.1017/aer.2016.7
https://doi.org/10.1017/aer.2016.7
Publikováno v:
Journal of Propulsion and Power. 32:121-133
Mixing characteristics of a Mach 2 elliptic jet, with rectangular tabs placed along the major and minor axes are studied, at different levels of nozzle expansion. At all the pressure ratios, the jet with tabs along the minor axis experiences better m
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::77b42e01959858b439831a5b50b77751
https://doi.org/10.2514/1.b35877
https://doi.org/10.2514/1.b35877
Autor:
G. Kailash, S. M. Aravindh Kumar
Publikováno v:
IOP Conference Series: Materials Science and Engineering. 912:022012
The present experimental study aims at investigating the effect of fluidic injection by means of air tabs on the core of circular and square sonic jets issuing from orifice at different levels of underexpansion. The experiments were conducted by vary
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::94d311866c7ee4a2059c03d44cc274ce
https://doi.org/10.1088/1757-899x/912/2/022012
https://doi.org/10.1088/1757-899x/912/2/022012