Add to ORKGThe report concerns: 1. Tuning of the aeroacoustic transonic model of the VEGA launcher;2. Tuning of the aeroacoustic supersonic model of the VEGA launcher;3. Extrapolation to flight condition of wind tunnel aeroacoustic transonic data;4. Extrapolation to flight condition of wind tunnel aeroacoustic supersonic data
This report describes a half-empirical model dealing with the sound radiation of modern turbofan eng...
The verification of a space launcher at the design level is a complex issue because of (i) the lack ...
A semiempirical maximum overall sound pressure level (OASPL) airframe noise model was derived. Noise...
The report concerns: 1. Tuning of the aeroacoustic transonic model of the VEGA launcher;2. Tuning o...
This work describes the main aspects of the extended experimental campaign aimed atthe characterizat...
The aeroacoustic environment created by the external aerodynamics around the VEGA launcher has to be...
VEGA, the future European small launch vehicle, is a single-body launcher composed of three solid-pr...
The present report concerns mainly with the analysis of the experimental data obtained in the supers...
An extensive wind tunnel test campaign devoted to the characterization of the aerodynamic and aeroac...
Aircraft noise is probably the most dominating contribution to community noise annoyance. The most e...
The German Aerospace Center has launched an internal project to assess the noise impact associated w...
abstract: At lift-off, a launch vehicle has to withstand a severe acoustic environment, induced by r...
One of the most critical regulatory issues related to supersonic flight arises from limitations impo...
PDFTech ReportDOT-VNTSC-RITA-FAA-09-02HMMH report no. 302920NoiseEnvironmental impactsEnvironmental ...
This paper proposes a preliminary subsonic aircraft and engine noise assessment framework, capable o...
This report describes a half-empirical model dealing with the sound radiation of modern turbofan eng...
The verification of a space launcher at the design level is a complex issue because of (i) the lack ...
A semiempirical maximum overall sound pressure level (OASPL) airframe noise model was derived. Noise...
The report concerns: 1. Tuning of the aeroacoustic transonic model of the VEGA launcher;2. Tuning o...
This work describes the main aspects of the extended experimental campaign aimed atthe characterizat...
The aeroacoustic environment created by the external aerodynamics around the VEGA launcher has to be...
VEGA, the future European small launch vehicle, is a single-body launcher composed of three solid-pr...
The present report concerns mainly with the analysis of the experimental data obtained in the supers...
An extensive wind tunnel test campaign devoted to the characterization of the aerodynamic and aeroac...
Aircraft noise is probably the most dominating contribution to community noise annoyance. The most e...
The German Aerospace Center has launched an internal project to assess the noise impact associated w...
abstract: At lift-off, a launch vehicle has to withstand a severe acoustic environment, induced by r...
One of the most critical regulatory issues related to supersonic flight arises from limitations impo...
PDFTech ReportDOT-VNTSC-RITA-FAA-09-02HMMH report no. 302920NoiseEnvironmental impactsEnvironmental ...
This paper proposes a preliminary subsonic aircraft and engine noise assessment framework, capable o...
This report describes a half-empirical model dealing with the sound radiation of modern turbofan eng...
The verification of a space launcher at the design level is a complex issue because of (i) the lack ...
A semiempirical maximum overall sound pressure level (OASPL) airframe noise model was derived. Noise...