NASA SP-8072 Acoustics Loads Generate by the Propulsion System
(Alternate SP-8072 link)
The liftoff analysis has been added to the GUI package at: Vibrationdata Matlab GUI
The function can be accessed via:
>> vibrationdata > Miscellaneous Functions I > Acoustics Vibroacoustics & SEA > acoustics > Launch Vehicle Liftoff Acoustics
Here is document which gives further details using an older C++ version: liftoff_notes.pdf
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The aerodynamic flow-induced pressure during the transonic and maximum dynamic pressure phases can be calculated using the follow tools:
Prediction of Sound Pressure Levels on Rocket Vehicles During Ascent: flow.pdf
This function can be accessed via:
>> vibrationdata > Miscellaneous Functions I > Acoustics Vibroacoustics & SEA > acoustics > Launch Vehicle Aerodynamic Flow
– Tom Irvine
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