Establishment of aeropropulsion mach 3.6 test facility for high speed combustor research (AIAA 2013-2624)
IR@NAL: CSIR-National Aerospace Laboratories, Bangalore
View Archive Info| Field | Value | |
| Title |
Establishment of aeropropulsion mach 3.6 test facility for high speed combustor research (AIAA 2013-2624)
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| Creator |
Manjunath, P
Sathiyamoorthy, K Venu, G Venkat Iyengar, S Jayaprakash, C Srinivas, J Prateesh Kumar, P |
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| Subject |
Aeronautics (General)
Aircraft Propulsion and Power |
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| Description |
National Aerospace Laboratories has recently established the Aeropropulsion Mach 3.6 test facility for experimental research on 'High Speed Combustors'. This is a blow down type test facility and simulates the combustor inlet conditions of Mach number and Temperature corresponding to the flight Mach number of 6 and an altitude of 25 km. The details of the facility, it's operation and flow characteristics have been described in this paper. The salient features of the control system of the facility has also been discussed. The facility was commissioned and operationalized in March 2012 and the flow conditions obtained at the test section are Mach number 3.6, total temperature 1700 K, pressure 18 bar with 12 s of effective test duration. This facility can be used as a semi-freejet test facility for the experimental research on the high speed combustors.
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| Date |
2013
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| Type |
Conference or Workshop Item
PeerReviewed |
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| Format |
application/pdf
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| Identifier |
http://nal-ir.nal.res.in/11977/1/AIAA%2D2013%2D2624.pdf
Manjunath, P and Sathiyamoorthy, K and Venu, G and Venkat Iyengar, S and Jayaprakash, C and Srinivas, J and Prateesh Kumar, P (2013) Establishment of aeropropulsion mach 3.6 test facility for high speed combustor research (AIAA 2013-2624). In: AIAA Ground Testing Conference, 24-27 June 2013, San Diego, CA. |
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| Relation |
http://dx.doi.org/10.2514/6.2013-2624
http://nal-ir.nal.res.in/11977/ |
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