An introduction to the first low boom prediction workshop is presented. The workshop objective will be to assess the state of the art for using computational fluid dynamics to predict near-field pressure signatures needed for accurate sonic boom propagations. Workshop participants will be supplied with 3 models, analysis of two will be required and the third optional. The models vary from a simple body of revolution to a complex full aircraft configuration with flow through nacelles. Participants will be supplied with computational meshes suitable for Euler analysis. Wind tunnel data will also be made available before the workshop for comparison with participant generated computational results. At the conclusion of the workshop, areas will be identified which require additional research and development to accurately predict low sonic boom near-field signatures.
[1]
John Morgenstern,et al.
Full Configuration Low Boom Model and Grids for 2014 Sonic Boom Prediction Workshop
,
2013
.
[2]
John M. Morgenstern,et al.
How to Accurately Measure Low Sonic Boom or Model Surface Pressures in Supersonic Wind Tunnels
,
2012
.
[3]
J. P. Mendoza,et al.
Some Effects of Wing Planform on Sonic Boom
,
2013
.
[4]
Donald C. Howe,et al.
Quiet Spike Near Field Flight Test Pressure Measurements with CFD Comparisons
,
2008
.
[5]
David H. Graham,et al.
Aerodynamic Design of Shaped Sonic Boom Demonstration Aircraft
,
2005
.
[6]
Spencer R. Fugal,et al.
Experimental Validations of a Low-Boom Aircraft Design
,
2013
.