This is a work-in-progress.
Here are some slide presentation with an emphasis on launch vehicles.
Equivalent Static Loads for Random Vibration & Alternate Link
Damping & Isolation & Alternate Link
Liftoff Vibroacoustics & Alternate Link
Ascent Vibroacoustics & Alternate Link
Launch Vehicle Pogo, Combustion Instability and Thrust Oscillation & Alternate Link
Launch Vehicle Statistical Energy Analysis & Alternate Link
Modal Testing, Part I & Alternate Link
The Matlab GUI package and additional slide presentations may be downloaded at:
Vibrationdata Matlab Signal Analysis & Structural Dynamics Package
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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 & Alternate Link
See also:
NASA SP-8072 Launch Vehicle Liftoff AcousticsÂ
Vibroacoustics/Statistical Energy Analysis
Non-Gaussian Acoustic Pressure Amplitudes in High-Intensity Sound Fields
Franken Method for Cylindrical Shells
NASA-HDBK-7005 Dynamic Environmental Criteria
NASA SP-5002 Load Analyses of Spacecraft and Payloads
NASA CR-1302 Summary of Random Vibration Prediction Procedures
Vibration Testing & Analysis Standard References
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Miscellaneous
Launch Vehicle Tip Over Analysis
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– Tom Irvine
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