Zobrazeno 1 - 7
of 7
pro vyhledávání: '"Suresh Chandra, Khandai"'
Publikováno v:
International Journal of Turbo & Jet-Engines; May2024, Vol. 41 Issue 2, p201-210, 10p
Publikováno v:
International Journal of Turbo & Jet-Engines. 39:331-342
This paper presents the numerical simulation of Mach 1.5 supersonic jet with perforated tabs. The jet with straight perforation tab was compared with jets having slanted perforated tabs of different diameters. The perforation angles were kept as 0°
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9e37029e666472efd6c26a19d03b3f83
https://doi.org/10.1515/tjj-2019-0015
https://doi.org/10.1515/tjj-2019-0015
Publikováno v:
International Journal of Turbo & Jet-Engines. 38:331-339
Control of Mach 1.8 circular jet with slanted perforated tabs is studied experimentally. Two sets of perforated tabs were used for this study. The perforation angles were 0° and 30° with respect to axis of the nozzle. The blockage areas of the tabs
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::90d294788840a9fe8afd9412b3a189c1
https://doi.org/10.1515/tjj-2018-0034
https://doi.org/10.1515/tjj-2018-0034
Publikováno v:
IOP Conference Series: Materials Science and Engineering. 912:022007
This project presents the design of a combustor with rotary vanes at the diffuser section and analyzing it’s turbulence and velocity characteristics. Rotary vanes with 2-blade, 4-blade and 8-blade configuration are analyzed and compared. The model
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::088bdd46a01f1a2e006d307e0799df59
https://doi.org/10.1088/1757-899x/912/2/022007
https://doi.org/10.1088/1757-899x/912/2/022007
Autor:
S. Devanandh, P. Hari Prasath, Suresh Chandra Khandai, G. Jesurajanishanth, G. Ezhilmaran, A. Arivazhagan
Publikováno v:
IOP Conference Series: Materials Science and Engineering. 912:022006
The project is about the computational study of Single Expansion Ramp Nozzle (SERN). A comparison is carried out for four different cowls of length 2h with initial arc radii of 0mm, 10mm, 20mm and 30mm. The ramp and the cowl are angled. The study ela
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::18e26c0afc6a202ea8c2a3bf015e58c8
https://doi.org/10.1088/1757-899x/912/2/022006
https://doi.org/10.1088/1757-899x/912/2/022006
Autor:
Suresh Chandra Khandai, S. Apoorva
Publikováno v:
Lecture Notes in Mechanical Engineering ISBN: 9789811327179
Nozzles constitute the exhaust system of jet engines. They are designed to regulate the flow properties to provide the required thrust force for all flight conditions. In the present work, the simulation of a de Laval nozzle outfitted with a throat s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4de75ae528cac3051ce4aa60cc869f25
https://doi.org/10.1007/978-981-13-2718-6_2
https://doi.org/10.1007/978-981-13-2718-6_2
Publikováno v:
International Journal of Mechanical and Industrial Engineering. :274-278
The present work deals with the computational study of the single expansion ramp nozzle (SERN) flows for the supersonic regime. Theoretical calculations are carried out for different geometries with certain assumptions. Based on the initial calculati
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::81de32f34a2b0feb79f08de3e99de90a
https://doi.org/10.47893/ijmie.2014.1170
https://doi.org/10.47893/ijmie.2014.1170