Experimental investigation of combined transpiration and film cooling for sintered metal porous struts. (May 2017)
- Record Type:
- Journal Article
- Title:
- Experimental investigation of combined transpiration and film cooling for sintered metal porous struts. (May 2017)
- Main Title:
- Experimental investigation of combined transpiration and film cooling for sintered metal porous struts
- Authors:
- Jiang, Pei-Xue
Huang, Gan
Zhu, Yinhai
Liao, Zhiyuan
Huang, Zheng - Abstract:
- Highlights: A combined transpiration and film cooling method was experimentally evaluated for protecting struts. Film cooling and transpiration cooling had little effect on the flow field stability. The combined cooling method effectively cools both the leading edge and other parts of the strut. Abstract: A combined transpiration and film cooling method was evaluated experimentally for protecting struts made of sintered stainless steel porous media with film holes on the leading edge in a supersonic wind tunnel. The combined cooling results were compared to standard transpiration cooling of the strut. Schlieren figures show that the film cooling and transpiration cooling had little effect on the flow field stability and the shock wave profiles around the struts for the present conditions. Standard transpiration cooling can protect most of the strut but cannot effectively cool the leading edge even with increased coolant injection pressures. The combined film and transpiration cooling effectively cools both the leading edge and other parts of the strut. Non-uniform coolant injection with higher injection pressures in the front cavity and lower injection pressures in the back cavity more effectively utilized the limited coolant flow. The average cooling efficiency of the front part of the strut increased from 25.7% for standard transpiration cooling to 37.9% for combined transpiration and film cooling with the same coolant consumption using the optimal non-uniform coolant flowHighlights: A combined transpiration and film cooling method was experimentally evaluated for protecting struts. Film cooling and transpiration cooling had little effect on the flow field stability. The combined cooling method effectively cools both the leading edge and other parts of the strut. Abstract: A combined transpiration and film cooling method was evaluated experimentally for protecting struts made of sintered stainless steel porous media with film holes on the leading edge in a supersonic wind tunnel. The combined cooling results were compared to standard transpiration cooling of the strut. Schlieren figures show that the film cooling and transpiration cooling had little effect on the flow field stability and the shock wave profiles around the struts for the present conditions. Standard transpiration cooling can protect most of the strut but cannot effectively cool the leading edge even with increased coolant injection pressures. The combined film and transpiration cooling effectively cools both the leading edge and other parts of the strut. Non-uniform coolant injection with higher injection pressures in the front cavity and lower injection pressures in the back cavity more effectively utilized the limited coolant flow. The average cooling efficiency of the front part of the strut increased from 25.7% for standard transpiration cooling to 37.9% for combined transpiration and film cooling with the same coolant consumption using the optimal non-uniform coolant flow distribution. … (more)
- Is Part Of:
- International journal of heat and mass transfer. Volume 108:Part A(2017)
- Journal:
- International journal of heat and mass transfer
- Issue:
- Volume 108:Part A(2017)
- Issue Display:
- Volume 108, Issue 1 (2017)
- Year:
- 2017
- Volume:
- 108
- Issue:
- 1
- Issue Sort Value:
- 2017-0108-0001-0000
- Page Start:
- 232
- Page End:
- 243
- Publication Date:
- 2017-05
- Subjects:
- Transpiration cooling -- Film cooling -- Strut
Heat -- Transmission -- Periodicals
Mass transfer -- Periodicals
Chaleur -- Transmission -- Périodiques
Transfert de masse -- Périodiques
Electronic journals
621.4022 - Journal URLs:
- http://www.sciencedirect.com/science/journal/00179310 ↗
http://www.elsevier.com/journals ↗ - DOI:
- 10.1016/j.ijheatmasstransfer.2016.12.014 ↗
- Languages:
- English
- ISSNs:
- 0017-9310
- Deposit Type:
- Legaldeposit
- View Content:
- Available online (eLD content is only available in our Reading Rooms) ↗
- Physical Locations:
- British Library DSC - 4542.280000
British Library DSC - BLDSS-3PM
British Library HMNTS - ELD Digital store - Ingest File:
- 573.xml