Zobrazeno 1 - 10
of 57
pro vyhledávání: '"Comandur Venkatesan"'
Publikováno v:
Journal of Aircraft. 56:1272-1280
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3e0235c2d1d512bfe03d827413cb761c
https://doi.org/10.2514/1.c035273
https://doi.org/10.2514/1.c035273
Autor:
T. Sakthivel, Comandur Venkatesan
Publikováno v:
Journal of Aircraft. 54:1595-1604
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::54d4a641f20cbdb47a855e2c9bda7d81
https://doi.org/10.2514/1.c034226
https://doi.org/10.2514/1.c034226
Autor:
Comandur Venkatesan, M. Rohin Kumar
Publikováno v:
The Aeronautical Journal. 121:637-659
For performance improvement and noise reduction, swept and anhedral tips have been incorporated in advanced-geometry rotor blades. While there are aerodynamic benefits to these advanced tip geometries, they come at the cost of complicated structural
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a82759bf7eadcb77bda1dcdc681b55eb
https://doi.org/10.1017/aer.2017.15
https://doi.org/10.1017/aer.2017.15
Autor:
T. Sakthivel, Comandur Venkatesan
Publikováno v:
The Aeronautical Journal. 121:553-575
The aim of the present study is to develop a relatively simple flight dynamic model which should have the ability to analyse trim, stability and response characteristics of a rotorcraft under various manoeuvring conditions. This study further address
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a7f734a69bbe5eeeed232f5956754f4c
https://doi.org/10.1017/aer.2017.8
https://doi.org/10.1017/aer.2017.8
Autor:
M. Rohin Kumar, Comandur Venkatesan
Publikováno v:
The Aeronautical Journal. 120:271-290
The influence of the blade geometric parameters on the structural dynamic characteristics, response and loads of a helicopter rotor under hover condition in a whirl tower was investigated. A general geometry was considered for the rotor blade which i
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::511fcc38f6c318774e7711298fcd63e8
https://doi.org/10.1017/aer.2015.11
https://doi.org/10.1017/aer.2015.11
Publikováno v:
AIAA Journal. 53:3116-3125
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::122b22f7c540be3eb28da41a70f219ed
https://doi.org/10.2514/1.j053635
https://doi.org/10.2514/1.j053635
Autor:
Comandur Venkatesan, G.S. Dutta
Publikováno v:
Journal of Sound and Vibration. 332:6913-6923
Experimental studies have been performed on elastomeric layered composites to characterize the nonlinearity in dynamic stiffness and specific damping energy, so that their performance can be enhanced as isolators. The present study is divided into tw
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cb9cf22cddc00e7cbf36677e71c7c8d7
https://doi.org/10.1016/j.jsv.2013.08.013
https://doi.org/10.1016/j.jsv.2013.08.013
Publikováno v:
Journal of Fluids and Structures. 43:402-427
A method is presented in this paper to predict cascade flutter under subsonic stalled flow condition in a quasi-steady manner. The ability to predict the occurrence of aeroelastic flutter is highly important from the compressor design point of view.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::20609cdbe114a66b4dd19d624e536a60
https://doi.org/10.1016/j.jfluidstructs.2013.09.004
https://doi.org/10.1016/j.jfluidstructs.2013.09.004
Autor:
Comandur Venkatesan, Puneet Singh
Publikováno v:
Journal of Aircraft. 50:1465-1480
Because of their potential for application in both civil and military sectors as well as the challenge in designing a tiny flying vehicle, micro aerial vehicles have attracted enormous attention. Several configurations of micro aerial vehicles are un
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ad3a52e629dd50f8fd11c6d5b7de9942
https://doi.org/10.2514/1.c031971
https://doi.org/10.2514/1.c031971
Publikováno v:
Journal of Aerospace Engineering. 26:555-570
Rotary wing aeroelasticity is a highly complex phenomenon involving coupling between flexible blade dynamics and unsteady aerodynamics including stall and unsteady wake effects. In this paper, a low-cost computational aeroelastic model including the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5b91b89767374700262060251bfc83b7
https://doi.org/10.1061/(asce)as.1943-5525.0000168
https://doi.org/10.1061/(asce)as.1943-5525.0000168