Zobrazeno 1 - 10
of 20
pro vyhledávání: '"Soumya Ranjan Nanda"'
Publikováno v:
International Journal of Aerospace Engineering, Vol 2017 (2017)
Current investigations solely focus on application of an impulse facility in diverse area of high-speed aerodynamics and structural mechanics. Shock tube, the fundamental impulse facility, is specially designed and calibrated for present objectives.
Externí odkaz:
https://doaj.org/article/0d911785ad764b47a857ee1f97f55356
Publikováno v:
Journal of Thermophysics and Heat Transfer. 36:108-117
The knowledge of surface heat flux over aerodynamic surfaces is highly desirable for high-speed applications. Impulse test facilities like shock tubes and shock tunnels are invariantly employed for...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::779476c5285d8a1ee2eb32bfe04fc92b
https://doi.org/10.2514/1.t6269
https://doi.org/10.2514/1.t6269
Autor:
Mohammed Ibrahim Sugarno, Rohit Panthi, Talluri Vamsi Krishna, Aqib Khan, Soumya Ranjan Nanda, Rakesh Kumar
Publikováno v:
Journal of Spacecraft and Rockets. 57:1414-1418
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6964aa7e94bdf2d2af91e89b646820dc
https://doi.org/10.2514/1.a34760
https://doi.org/10.2514/1.a34760
Publikováno v:
Journal of Thermal Science and Engineering Applications. 14
The present investigations provide a pathway for implementation of soft computing-based Adaptive Neuro-Fuzzy Inference System (ANFIS) technique for prediction of surface heat flux from short duration temperature measurement in shock tubes or shock tu
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4d20ae4c098f1cdb7373eb4664e53280
https://doi.org/10.1115/1.4051726
https://doi.org/10.1115/1.4051726
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 233:5310-5320
A blunt double-cone model, equipped with a three-component accelerometer or piezofilm-based force balance system, is tested in the IITB-Shock Tunnel at 0 º and 10 º angle of inclinations during force measurement experiments. Conventional accelerome
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a9784c09efa5f8db6654cb5841638319
https://doi.org/10.1177/0954410019845200
https://doi.org/10.1177/0954410019845200
Publikováno v:
Measurement. 134:773-780
A blunt bi-conic aluminum model, integrated with a three component accelerometer force balance system, is tested in the IITB-Shock Tunnel at various angle of inclinations with an intention to measure aerodynamic coefficients. Initially, Genetic Algor
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e9ed5eb3b997acc05aa2872c8870b97a
https://doi.org/10.1016/j.measurement.2018.11.007
https://doi.org/10.1016/j.measurement.2018.11.007
We experimentally investigate a partially shrouded sonic jet (a sonic free-jet shielded by a solid wall-extension on one side) exiting from a planar nozzle at two different nozzle pressure ratio ($\zeta=4$ and $5$). We experimentally show that the in
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b09d1b3d891fd39943ddce343dbe64a0
http://arxiv.org/abs/2102.07096
http://arxiv.org/abs/2102.07096
A detailed numerical study on the phenomenon of Shock Wave focusing in air is carried out. The focusing phenomenon is achieved with the help of a shock tube and a converging section attached to it. The planar shock generated inside the shock tube is
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::82f576e5f24b1a595a9ebd0454cbecb3
Publikováno v:
Aerospace Science and Technology. 123:107481
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5ae7171842185214e02b2f047d441983
https://doi.org/10.1016/j.ast.2022.107481
https://doi.org/10.1016/j.ast.2022.107481
Autor:
S. K. Karthick, Ashoke De, Aqib Khan, Soumya Ranjan Nanda, T. V. Krishna, M. Chaudhary, Ibrahim M. Sugarno
The present work aims to study the fluidic behavior on lateral confinement by placing side-walls on the planar plug nozzle through experiments. The study involves two cases of nozzle pressure ratio (NPR=3, 6), which correspond to over-expanded nozzle
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::42eb491928695d251de7546012ee5c34