15   Artículos

 
en línea
Lakshmi Narayana Phaneendra Peri, Antonella Ingenito and Paolo Teofilatto    
The goal of this paper is to investigate the aerodynamic and aerothermodynamic behavior of the Schiaparelli capsule after the deployment of a supersonic disk-gap-band (DGB) parachute during its re-entry phase into the Martian atmosphere. The novelty of t... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Oreste Russo, Andrea Aprovitola, Donato de Rosa, Giuseppe Pezzella and Antonio Viviani    
The efficiency increase that distributed propulsion could deliver for future hybrid-electric aircraft is in line with the urgent demand for higher aerodynamic performances and a lower environmental impact. Several consolidated proprietary tools (not alwa... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Valeriy Zapryagaev, Ivan Kavun and Nikolay Kiselev    
Using the example of studying the supersonic underexpanded jet initial section, the issue of interpreting the experimental visualization data and Pitot pressure measurement data using the results of numerical calculations (2d RANS k-? SST) is discussed. ... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
James Brind and Graham Pullan    
We quantify the sensitivity of turbine acoustic impedance to aerodynamic design parameters. Impedance boundary conditions are an influential yet uncertain parameter in predicting the thermoacoustic stability of gas turbine combustors. We extend the semi-... ver más

 
en línea
Valery Zapryagaev, Nikolay Kiselev and Dmitry Gubanov    
In the present paper, we give a brief overview of the studies of supersonic jet flows which were performed recently with the aim of gaining experimental data on the formation of the shock-wave structure and jet mixing layer in such flows. Considerable at... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Shahram Karami and Julio Soria    
The spatiotemporal dynamics of the coherent structures in an under-expanded supersonic impinging jet are studied using a spectral proper orthogonal decomposition technique. For this analysis, a large eddy simulation of an under-expanded supersonic imping... ver más
Revista: Aerospace    Formato: Electrónico

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