Characterization of Titan 3-D acoustic pressure spectra by least-squares fit to theoretical model

Details Characterization of Titan 3-D acoustic pressure spectra by least-squares fit to theoretical model Characterization of Titan 3-D acoustic pressure spectra by least-squares fit to theoretical model

Jan 1980

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1980bc...rept.....h&link_type=abstract

Interim Report Boston Coll., Chestnut Hill, MA.

Mathematics

Power Spectra, Rocket Exhaust, Rocket Launching, Titan 3 Launch Vehicle, Acoustics, Least Squares Method, Mathematical Models

Scientific paper

A theoretical model for the acoustic spectra of undeflected rocket
plumes is fitted to computed spectra of a Titan III-D at varying times
after ignition, by a least-squares method. Tests for the goodness of the
fit are made.

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