Large Civil Tiltrotor (LCTR2) interior noise predictions due to turbulent boundary layer excitation /

Bibliographic Details

Main Author:	Grosveld, Ferdinand W. (Author)
Corporate Author:	United States. National Aeronautics and Space Administration (sponsoring body.)
Format:	Government Document eBook
Language:	English
Published:	Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, June 2013.
Series:	NASA contractor report ; NASA CR-218005.
Subjects:	Acoustic properties. Finite element method. Turbulent boundary layer. Tilt rotor aircraft. Sound pressure. Frequency response.
Online Access:	https://purl.fdlp.gov/GPO/gpo53817 http://purl.fdlp.gov/GPO/gpo53817