International audienceA comparison of sonic boom propagation codes from NASA and ONERA was conducted using low-boom test cases from the 3rd AIAA Sonic Boom Prediction Workshop. Near-field pressures from two different shaped, low-boom demonstration aircraft concepts had been calculated with computational fluid dynamics codes and were used as starting signatures for the acoustic propagation analyses. In addition, atmospheric profiles from NOAA's Climate Forecast System Reanalysis database, including pressure, temperature, humidity, and winds as a function of altitude, were used to predict sonic booms propagating through realistic atmospheric conditions. The ground waveforms and derived loudness metrics were compared at regular intervals acros...
An extensive sonic boom propagation database with low- to normal-intensity booms (overpressures of 0...
International audienceSonic boom prediction is tackled within the EU projectRUMBLE. Its aim ...
Two wing/fuselage/nacelle/fin concepts were designed to check the validity and the applicability of ...
Dassault Aviation as a civil aircraft manufacturer is studying the feasibility of a supersonic busin...
A summary is provided for the propagation portion of the second AIAA Sonic Boom Workshop held Januar...
International audienceWhilst the interest of industry for a second generation (post-Concorde) large ...
Sonic Booms of two different bodies, a double cone configuration and a modified F-5E aircraft are pr...
Flight at speeds greater than the speed of sound is not permitted over land, primarily because of th...
This paper describes the NASA ARC program in sonic boom prediction methodologies. This activity supp...
Near-field pressure signatures were measured and computational predictions made for several sonic bo...
As the industry progresses towards realizing a commercial supersonic aircraft, the push to reduce no...
In this paper the comparison between two different numerical approaches for sonic boom evaluation is...
Volpe National Transportation Systems Center, Technical Reference Centerhttps://doi.org/10.2514/6.20...
International audienceSonic boom prediction is tackled within the EU projectRUMBLE. Its aim ...
to quantify subjective loudness response to boom signatures consisting of: (a) simulator reproductio...
An extensive sonic boom propagation database with low- to normal-intensity booms (overpressures of 0...
International audienceSonic boom prediction is tackled within the EU projectRUMBLE. Its aim ...
Two wing/fuselage/nacelle/fin concepts were designed to check the validity and the applicability of ...
Dassault Aviation as a civil aircraft manufacturer is studying the feasibility of a supersonic busin...
A summary is provided for the propagation portion of the second AIAA Sonic Boom Workshop held Januar...
International audienceWhilst the interest of industry for a second generation (post-Concorde) large ...
Sonic Booms of two different bodies, a double cone configuration and a modified F-5E aircraft are pr...
Flight at speeds greater than the speed of sound is not permitted over land, primarily because of th...
This paper describes the NASA ARC program in sonic boom prediction methodologies. This activity supp...
Near-field pressure signatures were measured and computational predictions made for several sonic bo...
As the industry progresses towards realizing a commercial supersonic aircraft, the push to reduce no...
In this paper the comparison between two different numerical approaches for sonic boom evaluation is...
Volpe National Transportation Systems Center, Technical Reference Centerhttps://doi.org/10.2514/6.20...
International audienceSonic boom prediction is tackled within the EU projectRUMBLE. Its aim ...
to quantify subjective loudness response to boom signatures consisting of: (a) simulator reproductio...
An extensive sonic boom propagation database with low- to normal-intensity booms (overpressures of 0...
International audienceSonic boom prediction is tackled within the EU projectRUMBLE. Its aim ...
Two wing/fuselage/nacelle/fin concepts were designed to check the validity and the applicability of ...