High Power Density Silicon Combustion Systems for Micro Gas Turbine Engines
By Christopher M. Spadaccini, Joosung J. Lee, S. P. Lukachko, I. Waitz, A. Mehra, Xin Zhang. 2003
152 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Computational Mechanics, Fluid Flow and Transfer Processes
View Paper: https://www.semanticscholar.org/paper/c801dc3bf990cbee750467c7e9f3ffab02f8cd38
How researchers see this paper
The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.
In Aerospace Engineering
- A. Epstein
- Luis A. Aguirre
- Leonardo A. B. Tôrres
- J. Chandrasekar
- Sarah Dennis
- Samuel S. Bernstein
- Xavier Vazhappilly Francis
- Publisher Taylor
In Computational Mechanics
In Fluid Flow and Transfer Processes
Citations in the corpus
- Millimeter-Scale, MEMS Gas Turbine Engines (2003, background): “A comparison between a modern aircraft engine combustor and a microengine is shown in Table 1 [31].”
- Ltd Registered in England and Wales Registered Number : 1072954 Registered office : (2004, background): “The mean residence time can be defined as the time a parcel of gas spends inside the combustor, its value estimated as the ratio between the mass of gas in the chamber volume, Vc q, and the mass flow rate, _ m (Spadaccini et al., 2003):”