Preliminary CFD analysis of the vortex hybrid rocket chamber and nozzle flow field

Author(s):  
William Knuth ◽  
Daniel Gramer ◽  
Martin Chiaverini ◽  
J. Sauer ◽  
R. Whitesides ◽  
...  
2021 ◽  
Vol 98 (10) ◽  
pp. 100159
Author(s):  
Cholu Kwon ◽  
Un song Pak ◽  
Chung myong Kim ◽  
Chen ho Paek

1986 ◽  
Vol 108 (2) ◽  
pp. 269-274
Author(s):  
R. G. Williamson ◽  
S. H. Moustapha ◽  
J. P. Huot

Two nozzle designs, involving the same low aspect ratio, high turning angle vanes, and differing in outer wall contour, were tested over a range of exit Mach numbers up to supersonic values. The experiments were conducted on a large-scale, full annular configuration with and without a representative rotor downstream. Nozzle performance was found to be significantly affected by rotor operation, the influence depending on the detailed characteristics of the nozzle flow field, as well as on the design and operation of the rotor itself. It is suggested that performance evaluation of low aspect ratio nozzles of high turning angle may require appropriate testing with a rotor.


2010 ◽  
Vol 240 (2) ◽  
pp. 352-363 ◽  
Author(s):  
S. Tóth ◽  
A. Aszódi
Keyword(s):  

2019 ◽  
Author(s):  
Nicola Lucarelli ◽  
Elise Eckman ◽  
Kevin J. Disotell

2015 ◽  
Vol 2015 (0) ◽  
pp. _0509-1_-_0509-2_
Author(s):  
Harutaka OE ◽  
Hiroya MAMORI ◽  
Yasutada TANABE ◽  
Makoto YAMAMOTO ◽  
Hideaki SUGAWARA

2016 ◽  
Vol 2016.53 (0) ◽  
pp. _1312-1_-_1312-5_
Author(s):  
Yuki OHTA ◽  
Yosuke KIMURA ◽  
Yusuke KATAYAMA ◽  
Shouichiro IIO ◽  
Yoshihide MORI ◽  
...  

2009 ◽  
Vol 74 (638) ◽  
pp. 481-488 ◽  
Author(s):  
Tomohiro KOBAYASHI ◽  
Kazunobu SAGARA ◽  
Toshio YAMANAKA ◽  
Hisashi KOTANI ◽  
Shogo TAKEDA ◽  
...  

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