This paper presents an experimental investigation of the aerodynamic and thermal characteristics of a round jet of hot air, injected through a nozzle into a parallel air flow, simulating a hot streak. Experiments were performed by imposing the same total pressure, established by means of a five-hole probe, for the mainstream and the jet at nozzle exit. Time-averaged temperatures at different points over planes downstream of the nozzle exit section were measured by thermocouple rakes. Experimental data, presented in a non-dimensional form, provide a representation not correlated to individual maximum jet temperature and Reynolds number, in the respective fields of variation. The attenuation of the hot jet strength is reported as a function of the normalized axial coordinate for the various operating conditions considered. Results obtained for the hot jet discharged into a parallel flow are compared with data obtained for the hot jet spreading into stagnant air.
Satta, F., & Tanda, G. (2016). Aerodynamic and Thermal Characteristics of a Hot Jet in Parallel Flow. Journal of Applied Fluid Mechanics, 9(5), 2105-2110. doi: 10.18869/acadpub.jafm.68.236.25087
MLA
F. Satta; G. Tanda. "Aerodynamic and Thermal Characteristics of a Hot Jet in Parallel Flow". Journal of Applied Fluid Mechanics, 9, 5, 2016, 2105-2110. doi: 10.18869/acadpub.jafm.68.236.25087
HARVARD
Satta, F., Tanda, G. (2016). 'Aerodynamic and Thermal Characteristics of a Hot Jet in Parallel Flow', Journal of Applied Fluid Mechanics, 9(5), pp. 2105-2110. doi: 10.18869/acadpub.jafm.68.236.25087
VANCOUVER
Satta, F., Tanda, G. Aerodynamic and Thermal Characteristics of a Hot Jet in Parallel Flow. Journal of Applied Fluid Mechanics, 2016; 9(5): 2105-2110. doi: 10.18869/acadpub.jafm.68.236.25087