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Comparison of Spatial Correlation Parameters between Full and Model Scale Launch VehiclesThe current vibro-acoustic analysis tools require specific spatial correlation parameters as input to define the liftoff acoustic environment experienced by the launch vehicle. Until recently these parameters have not been very well defined. A comprehensive set of spatial correlation data were obtained during a scale model acoustic test conducted in 2014. From these spatial correlation data, several parameters were calculated: the decay coefficient, the diffuse to propagating ratio, and the angle of incidence. Spatial correlation data were also collected on the EFT-1 flight of the Delta IV vehicle which launched on December 5th, 2014. A comparison of the spatial correlation parameters from full scale and model scale data will be presented.
Document ID
20170000434
Acquisition Source
Marshall Space Flight Center
Document Type
Abstract
Authors
Kenny, Jeremy
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Giacomoni, Clothilde
(Jacobs Engineering and Science Services and Skills Augmentation Group (ESSSA) Huntsville, AL, United States)
Date Acquired
January 13, 2017
Publication Date
November 25, 2016
Subject Category
Acoustics
Report/Patent Number
M16-5412
Report Number: M16-5412
Meeting Information
Meeting: Acoustical Society of America
Location: Honolulu, HI
Country: United States
Start Date: November 28, 2016
End Date: December 2, 2016
Sponsors: Acoustical Society of America
Funding Number(s)
CONTRACT_GRANT: NNM1ZAA41C
Distribution Limits
Public
Copyright
Public Use Permitted.
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