Abstract
When a vehicle such as a rocket moves through atmospheric turbulence of large spatial scale, the pressure is at any instant essentially uniform over the entire vehicle surface, but this uniform pressure changes randomly in time. Measurements of gust load spectra provide estimates of the significant parameters describing the pressure field. The modal response of a simple elastic system and the sound reradiated by this system are determined. Atmospheric turbulence appears to be a potentially significant noise source in flight vehicles. [Supported by Wright Air Development Center under Contract No. AF 33(616)-6217.]
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
