(Maximum 200 words) A laboratory study was conducted to determine the effects of sonic boom signature shaping on subjective loudness and acceptability. The study utilized the sonic boom simulator at the Langley Research Center. A wide range of symmetrical, front-shock-minimized signature shapes were investigated together with a limited number of asymmetrical signatures. Subjective loudness judgments were obtained from 60 test subjects by using an 11-point numerical category scale. Acceptability judgments were obtained using the method of constant stimuli. Results were used to assess the relative predictive ability of several noise metrics, determine the loudness benefits of detailed boom shaping, and derive laboratory sonic boom acceptabil...
National audienceThe aim of our work is to study loudness and annoyance of sonic boom. For that a sp...
Three experiments were conducted to determine subjective equivalence of aircraft subsonic flyover no...
A laboratory study was conducted for the following reasons: (1) to investigate the application of ma...
A laboratory study was conducted to determine the effects of sonic boom signature shaping on subject...
this paper is to quantify subjective loudness response to a set of signatures selected from those re...
The purpose of this paper is to summarize the most recent sonic boom laboratory studies performed at...
Two laboratory experiments were conducted to quantify the subjective response of people to simulated...
INTRODUCTION NASA Langley Research Center is supporting NASA High-Speed Research Program efforts to ...
Manufacturers of business jets have expressed interest in designing and building a new generation of...
The NASA Langley Research Center's sonic boom apparatus was used in an experimental study to quantif...
The Sonic Boom Simulator of the Langley Research Center was used to quantify subjective loudness res...
this paper is to present the results of three experiments recently conducted at NASA Langley Researc...
A sonic boom simulator at NASA Langley Research Center has been constructed for research on human re...
OAM report.PDFTech ReportFAA-AM-74-9DOT/FAA/AM-74/9Sonic boomNoiseAnnoyancePerformanceAdaptation (Ps...
Various studies were conducted by NASA and others on the practical limitations of sonic boom signatu...
National audienceThe aim of our work is to study loudness and annoyance of sonic boom. For that a sp...
Three experiments were conducted to determine subjective equivalence of aircraft subsonic flyover no...
A laboratory study was conducted for the following reasons: (1) to investigate the application of ma...
A laboratory study was conducted to determine the effects of sonic boom signature shaping on subject...
this paper is to quantify subjective loudness response to a set of signatures selected from those re...
The purpose of this paper is to summarize the most recent sonic boom laboratory studies performed at...
Two laboratory experiments were conducted to quantify the subjective response of people to simulated...
INTRODUCTION NASA Langley Research Center is supporting NASA High-Speed Research Program efforts to ...
Manufacturers of business jets have expressed interest in designing and building a new generation of...
The NASA Langley Research Center's sonic boom apparatus was used in an experimental study to quantif...
The Sonic Boom Simulator of the Langley Research Center was used to quantify subjective loudness res...
this paper is to present the results of three experiments recently conducted at NASA Langley Researc...
A sonic boom simulator at NASA Langley Research Center has been constructed for research on human re...
OAM report.PDFTech ReportFAA-AM-74-9DOT/FAA/AM-74/9Sonic boomNoiseAnnoyancePerformanceAdaptation (Ps...
Various studies were conducted by NASA and others on the practical limitations of sonic boom signatu...
National audienceThe aim of our work is to study loudness and annoyance of sonic boom. For that a sp...
Three experiments were conducted to determine subjective equivalence of aircraft subsonic flyover no...
A laboratory study was conducted for the following reasons: (1) to investigate the application of ma...