In support of ongoing efforts to bring commercial supersonic flight to the public, the Sonic Booms in Atmospheric Turbulence (SonicBAT) flight test was conducted at NASA Armstrong Flight Research Center. During this test, airborne sonic boom measurements were made using an instrumented TG-14 motor glider, called the Airborne Acoustic Measurement Platform (AAMP).During the flight program, the AAMP was consistently able to measure the sonic boom wave that was reflected off of the ground, in addition to the incident wave, resulting in the creation of a completely unique data set of airborne sonic boom reflection measurements. This paper focuses on using this unique data set to investigate the ability of sonic boom modeling software to calculat...
Exposure pattern development, propagation through inhomogeneous atmosphere, and effects on people an...
Supersonic flights can greatly shorten the flight time in the world and provide convenience for peop...
this paper is to quantify subjective loudness response to a set of signatures selected from those re...
One of the current impediments to the establishment of supersonic transports as a viable part of the...
The results of sonic boom research studies are presented. The purpose of the studies was as follows:...
The objectives of the Sonic Booms in Atmospheric Turbulence (SonicBAT) Program were to develop and v...
An extensive sonic boom propagation database with low- to normal-intensity booms (overpressures of 0...
Flight at speeds greater than the speed of sound is not permitted over land, primarily because of th...
Before beginning this presentation, it is appropriate to acknowledge the sincere interest and financ...
The sonic boom flight test program conducted at Jackass Flats, Nevada, during the summer and fall of...
This study deals with the potential audibility of sonic booms from supersonic aircraft at the ground...
INTRODUCTION The proposed development of a second-generation supersonic commercial transport has re...
Sonic booms generated by the X-15 airplane flying at Mach numbers of 3.5 and 4.8 were measured. The ...
International audienceSonic boom prediction is tackled within the EU projectRUMBLE. Its aim ...
The topics discussed include the following: atmospheric turbulence; BOOMFILE Database description; B...
Exposure pattern development, propagation through inhomogeneous atmosphere, and effects on people an...
Supersonic flights can greatly shorten the flight time in the world and provide convenience for peop...
this paper is to quantify subjective loudness response to a set of signatures selected from those re...
One of the current impediments to the establishment of supersonic transports as a viable part of the...
The results of sonic boom research studies are presented. The purpose of the studies was as follows:...
The objectives of the Sonic Booms in Atmospheric Turbulence (SonicBAT) Program were to develop and v...
An extensive sonic boom propagation database with low- to normal-intensity booms (overpressures of 0...
Flight at speeds greater than the speed of sound is not permitted over land, primarily because of th...
Before beginning this presentation, it is appropriate to acknowledge the sincere interest and financ...
The sonic boom flight test program conducted at Jackass Flats, Nevada, during the summer and fall of...
This study deals with the potential audibility of sonic booms from supersonic aircraft at the ground...
INTRODUCTION The proposed development of a second-generation supersonic commercial transport has re...
Sonic booms generated by the X-15 airplane flying at Mach numbers of 3.5 and 4.8 were measured. The ...
International audienceSonic boom prediction is tackled within the EU projectRUMBLE. Its aim ...
The topics discussed include the following: atmospheric turbulence; BOOMFILE Database description; B...
Exposure pattern development, propagation through inhomogeneous atmosphere, and effects on people an...
Supersonic flights can greatly shorten the flight time in the world and provide convenience for peop...
this paper is to quantify subjective loudness response to a set of signatures selected from those re...