← Back to Browse
Analytical studies of boundary layer generated aircraft interior noise

Analytical studies of boundary layer generated aircraft interior noise

by M. S. Howe

First published: 1997

Subjects

Fuselages Turbulent flow Turbulent boundary layer Boundary layers Sound waves Vibration Wall pressure Subsonic flow Aircraft noise Pressure oscillations
Read on Open Library More by M. S. Howe

Related Books

Two-dimensional aerodynamic characteristics of several polygon-shaped cross-sectional models applicable to helicopter fuselages

Two-dimensional aerodynamic characteristics of several polygon-shaped cross-sectional models applicable to helicopter fuselages

Henry L. Kelley

19924 ed.
An in-flight investigation of a twin fuselage configuration in approach and landing

An in-flight investigation of a twin fuselage configuration in approach and landing

N. Weingarten

19843 ed.
Calculation of three-dimensional, inviscid supersonic, steady flows

Calculation of three-dimensional, inviscid supersonic, steady flows

Gino Moretti

19825 ed.
A possibility of avoiding surface roughness due to insects

A possibility of avoiding surface roughness due to insects

Franz Xaver Wortmann

19843 ed.
An in-flight investigation of a twin fuselage configuration in approach and landing

An in-flight investigation of a twin fuselage configuration in approach and landing

N Weingarten

19842 ed.
Navier-Stokes and potential theory solutions for a helicopter fuselage and comparison with experiment

Navier-Stokes and potential theory solutions for a helicopter fuselage and comparison with experiment

Mark S. Chaffin

19945 ed.
Vibro-acoustics modal testing at NASA Langley Research Center

Vibro-acoustics modal testing at NASA Langley Research Center

Richard S. Pappa

19995 ed.
Water-tunnel study results of a TF/A-18 and F/A-18 canopy flow visualization

Water-tunnel study results of a TF/A-18 and F/A-18 canopy flow visualization

Steven A. Johnson

19904 ed.