Zobrazeno 1 - 10
of 69
pro vyhledávání: '"Hypersonic Shock Tunnel (HST2)"'
Publikováno v:
Shock Waves ISBN: 9783540224976
The drag and lift coefficients for a viscous optimized Mach 6 conical waverider has been measured using an accelerometer force balance system in the IISc hypersonic shock tunnel. A rubber bush placed in between the waverider model and the steel sting
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::77fd52d093f3d3c075e05f40f5640d24
https://doi.org/10.1007/978-3-540-27009-6_49
https://doi.org/10.1007/978-3-540-27009-6_49
Publikováno v:
IndraStra Global.
The drag and lift coefficients for a viscous optimized Mach 6 conical waverider has been measured using an accelerometer force balance system in the IISc hypersonic shock tunnel. A rubber bush placed in between the waverider model and the steel sting
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=issn23813652::1a97eb499e8d3ce6ddfc32e640f2135f
http://eprints.iisc.ac.in/43741/1/Force_measurements.pdf
http://eprints.iisc.ac.in/43741/1/Force_measurements.pdf
Autor:
Nagashetty, K
In the flying field of space transportation domain, the increased efforts involving design and development of hypersonic flight for space missions is on toe to provide the optimum aerothermodynamic design data to satisfy mission requirements. Aerothe
Externí odkaz:
http://hdl.handle.net/2005/3195
http://etd.ncsi.iisc.ernet.in/abstracts/4067/G26579-Abs.pdf
http://etd.ncsi.iisc.ernet.in/abstracts/4067/G26579-Abs.pdf
Autor:
Philip, Sarah Jobin
Aerodynamic cavities are common features on hypersonic vehicles which are caused in both large and small scale features like surface defects, pitting, gap in joints etc. In the hypersonic regime, the presence of such cavities alters the flow phenomen
Externí odkaz:
http://etd.iisc.ernet.in/2005/3900
http://etd.iisc.ernet.in/abstracts/4775/G25303-Abs.pdf
http://etd.iisc.ernet.in/abstracts/4775/G25303-Abs.pdf
Autor:
Thakur, Ruchi
One of the characteristics of the high speed ows over blunt bodies is the detached shock formed in front of the body. The distance of the shock from the stagnation point measured along the stagnation streamline is termed as the shock stand o distance
Externí odkaz:
http://etd.iisc.ernet.in/2005/3848
http://etd.iisc.ernet.in/abstracts/4720/G27111-Abs.pdf
http://etd.iisc.ernet.in/abstracts/4720/G27111-Abs.pdf
Autor:
Reddeppa, P
Knowledge of flow separation is very essential for proper understanding of both external and internal aerothermodynamics of bodies. Because of unique flow features such as thick boundary layers, merged shock layers, strong entropy layers, flow separa
Externí odkaz:
http://hdl.handle.net/2005/586
Autor:
Srinath, S
The emerging and competitive environment in the space technology requires the improvements in the capability of aerodynamic vehicles. This leads to the analysis in drag reduction of the vehicle along with the minimized heat transfer rate. Using forwa
Externí odkaz:
http://hdl.handle.net/2005/1116
Autor:
Joarder, Ratan
For flights beyond Mach 6 ramjets are inefficient engines due to huge total pressure loss in the normal shock systems, combustion conditions that lose a large fraction of the available chemical energy due to dissociation and high structural loads. Ho
Externí odkaz:
http://hdl.handle.net/2005/1005
Autor:
Venukumar, Balla1 laser@aero.iisc.ernet.in, Reddy, K. P. J.1 laser@aero.iisc.ernet.in
Publikováno v:
Sādhanā: Academy Proceedings in Engineering Sciences. Feb/Apr2007, Vol. 32 Issue 1/2, p123-131. 9p. 2 Color Photographs, 2 Black and White Photographs, 4 Diagrams, 1 Chart, 2 Graphs.
Publikováno v:
Current Science (00113891). 1/10/2007, Vol. 92 Issue 1, p56-60. 5p. 2 Black and White Photographs, 2 Diagrams, 1 Chart, 3 Graphs.