ESDU 07001:2011
$126.75
Noise Transmission into Aircraft Cabins
| Published By | Publication Date | Number of Pages |
| ESDU | 2011-03 | NA |
ESDU 07001 provides a means of estimating the reduction in noise
levels through a fuselage wall with or without cabin wall trim. The
prediction method is based on the power flow approach and is
intended for application to the radiation of both tonal and
broadband noise from various types of aircraft engines into the
aircraft cabin.
The program requires as input the cabin geometry, material
properties, details about trim properties and acoustic and
structural loss factors. The user has the option of using either
one of three provided cabin wall trim models with any combination
of three trim elements with up to a maximum number of ten elements.
A routine to estimate acoustic loss factors can be employed if
required.
Two additional programs to facilitate the generation of input
files are included.
Related products
-
ESDU TN 07007:2012
Incompressible Flow Through Orifice Plates – a Review of the Data in the Literature Published…
-
BSI PD IEC/TS 62686-1:2015
Process management for avionics. Electronic components for aerospace, defence and high performance (ADHP) applications –…
-
ESDU 07003:2011
Modelling of wing viscous drag coefficient in shock-free attached flow Published By Publication Date Number…
-
ESDU 07004:2010
Flow in Rotating Components – Discs, Cylinders and Cavities Published By Publication Date Number of…
-
ESDU 00001:2015
Aerodynamics Series: Record of Documents Published By Publication Date Number of Pages ESDU 2015-08-01 45
-
ESDU 09001:2019
Aerodynamics and Aero-Acoustics of Rectangular Planform Cavities – Part IIIC: Alleviation of Unsteady Flow Effects…
-
ESDU 05001:2016
Prediction of Combustor Noise from Gas Turbine Engines Published By Publication Date Number of Pages…
-
ESDU 07002:2011
Wing viscous drag coefficient in shock-free attached flow Published By Publication Date Number of Pages…