To compare the behaviour of regeneration and wave rotor techniques in jet propulsion a numerical code has been developed and some interesting results has been obtained. The code simulates the thermodynamic behaviour of different jet engines (simple turbojet, turbofan and turboprop), for different operative conditions and engine parameters. The numerical analysis has been carried on considering several efficiencies of regeneration and wave rotor pressure ratio. The simulations have put in evidence the effect of regeneration particularly on the specific fuel consumption and the effect of wave rotor mainly on the specific power. © 2001 The American Institute of Aeronautics and Astronautics Inc. All rights reserved.

COMPARISON BETWEEN WAVE ROTOR AND REGENERATIVE CYCLES IN PROPULSION / Antonini, F; Gamma, Fausto. - (2001). (Intervento presentato al convegno 37th Joint Propulsion Conference and Exhibit 2001 tenutosi a Salt Lake City, UT; United States).

COMPARISON BETWEEN WAVE ROTOR AND REGENERATIVE CYCLES IN PROPULSION

GAMMA, Fausto
2001

Abstract

To compare the behaviour of regeneration and wave rotor techniques in jet propulsion a numerical code has been developed and some interesting results has been obtained. The code simulates the thermodynamic behaviour of different jet engines (simple turbojet, turbofan and turboprop), for different operative conditions and engine parameters. The numerical analysis has been carried on considering several efficiencies of regeneration and wave rotor pressure ratio. The simulations have put in evidence the effect of regeneration particularly on the specific fuel consumption and the effect of wave rotor mainly on the specific power. © 2001 The American Institute of Aeronautics and Astronautics Inc. All rights reserved.
2001
37th Joint Propulsion Conference and Exhibit 2001
Engine parameter;Jet propulsion;Numerical code
04 Pubblicazione in atti di convegno::04b Atto di convegno in volume
COMPARISON BETWEEN WAVE ROTOR AND REGENERATIVE CYCLES IN PROPULSION / Antonini, F; Gamma, Fausto. - (2001). (Intervento presentato al convegno 37th Joint Propulsion Conference and Exhibit 2001 tenutosi a Salt Lake City, UT; United States).
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11573/186987
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