Combined quadrupole-dipole model for inlet flow distortion noise from a subsonic fan / by Marvin E. Goldstein, James H. Dittmar, and Thomas F. Gelder.

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Bibliographic Details
Online Access:	Search for the full-text version of this title in HathiTrust
Main Author:	Goldstein, Marvin E.
Corporate Authors:	Lewis Research Center, United States. National Aeronautics and Space Administration
Other Authors:	Dittmar, James H., Gelder, Thomas F.
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1974.
Series:	NASA technical note ; D-7676.
Subjects:	Airplanes > Turbofan engines > Noise > Mathematical models. Airplanes > Turbojet engines > Air intakes > Noise > Mathematical models. Gas-turbines > Aerodynamics > Mathematical models. Air ducts > Acoustic properties > Mathematical models. Air ducts > Aerodynamics > Mathematical models.

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Holdings details from Norlin Library - Government Information - US
Call Number:	NAS 1.14:D-7676
NAS 1.14:D-7676	Available Place a Hold