IHS ESDU Noise transmission into aircraft cabins. Addendum: Estimation of section properties of fuselage stiffeners. 07001 Addendum

Description
This Addendum to ESDU 07001 includes a computer program to calculate section properties of fuselage stiffeners rapidly. These properties are required input for Program A0701 which estimates the noise reduction through cabin walls. The cross-section of a stiffener must be divided into a set of elements, each of rectangular cross-sectional area. The width, height and distance of centroid from the skin surface are then required input for each element. The program then returns values of the cross-sectional area, the distance of the centroid from the skin surface, the second moment of area and the torsional constant for the entire section.
Description
This Addendum to ESDU 07001 includes a computer program to calculate section properties of fuselage stiffeners rapidly. These properties are required input for Program A0701 which estimates the noise reduction through cabin walls. The cross-section of a stiffener must be divided into a set of elements, each of rectangular cross-sectional area. The width, height and distance of centroid from the skin surface are then required input for each element. The program then returns values of the cross-sectional area, the distance of the centroid from the skin surface, the second moment of area and the torsional constant for the entire section.

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Noise transmission into aircraft cabins. Addendum: Estimation of section properties of fuselage stiffeners. - 07001 Addendum - IHS ESDU
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Noise transmission into aircraft cabins. Addendum: Estimation of section properties of fuselage stiffeners.
07001 Addendum
Noise transmission into aircraft cabins. Addendum: Estimation of section properties of fuselage stiffeners. 07001 Addendum
This Addendum to ESDU 07001 includes a computer program to calculate section properties of fuselage stiffeners rapidly. These properties are required input for Program A0701 which estimates the noise reduction through cabin walls. The cross-section of a stiffener must be divided into a set of elements, each of rectangular cross-sectional area. The width, height and distance of centroid from the skin surface are then required input for each element. The program then returns values of the cross-sectional area, the distance of the centroid from the skin surface, the second moment of area and the torsional constant for the entire section.

This Addendum to ESDU 07001 includes a computer program to calculate section properties of fuselage stiffeners rapidly. These properties are required input for Program A0701 which estimates the noise reduction through cabin walls. The cross-section of a stiffener must be divided into a set of elements, each of rectangular cross-sectional area. The width, height and distance of centroid from the skin surface are then required input for each element. The program then returns values of the cross-sectional area, the distance of the centroid from the skin surface, the second moment of area and the torsional constant for the entire section.

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Technical Specifications

  IHS ESDU
Product Category Standards and Technical Documents
Product Number 07001 Addendum
Product Name Noise transmission into aircraft cabins. Addendum: Estimation of section properties of fuselage stiffeners.
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