Zobrazeno 1 - 10
of 10
pro vyhledávání: '"Srisha Rao M V"'
Autor:
Kanishka Deepak, Aaditya U Wangikar, Chathura G R, Sanmukh Sharad Khadtare, Anagha G Rao, Yatin Yogesh, Mukesh M, Srisha Rao M V
Publikováno v:
2022 IEEE Aerospace Conference (AERO).
Publikováno v:
Measurement Science and Technology. 33:125111
In this work, we have demonstrated the use of fiber Bragg grating (FBG) sensors for simultaneous measurement of wall static pressure and temperature in a supersonic ejector. Supersonic ejectors are ground-based high-speed aerodynamic test facilities
Autor:
Srisha Rao, M V
A supersonic ejector is used to pump a secondary gas using a supersonic primary gas flow by augmentation of momentum and energy in a variable area duct. The internal compressible flow through an ejector has many complex gas dynamic features, like com
Externí odkaz:
http://etd.iisc.ernet.in/2005/3402
http://etd.iisc.ernet.in/abstracts/4268/G25868-Abs.pdf
http://etd.iisc.ernet.in/abstracts/4268/G25868-Abs.pdf
Autor:
Srisha Rao, M. V., Jagadeesh, G.
Publikováno v:
28th International Symposium on Shock Waves; 2012, p965-971, 7p
Publikováno v:
28th International Symposium on Shock Waves; 2012, p867-872, 6p
Publikováno v:
Journal of Mechanical Engineering / Strojniški Vestnik. 2018, Vol. 64 Issue 2, p95-104. 10p.
Publikováno v:
International Journal of Aerospace Innovations. Dec2012, Vol. 4 Issue 3/4, p75-84. 10p.
Publikováno v:
29th International Symposium on Shock Waves 2; 2015, p1621-1633, 13p
Publikováno v:
29th International Symposium on Shock Waves 1; 2015, p807-819, 13p
Autor:
Thomas B. Gatski, Jean-Paul Bonnet
Compressibility, Turbulence and High Speed Flow introduces the reader to the field of compressible turbulence and compressible turbulent flows across a broad speed range, through a unique complimentary treatment of both the theoretical foundations an