Longitudinal Impact Test of a Transport Airframe Section

Wade, Barry; Johnson, Dick

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Longitudinal Impact Test of a Transport Airframe Section

1988-07-01
By Wade, Barry ; Johnson, Dick

File Language:

English

[PDF - 17.95 MB]

Details

Creators:

Wade, Barry ; Johnson, Dick
Corporate Creators:

Transportation Research Center Inc.
Corporate Contributors:

United States. Department of Transportation. Federal Aviation Administration. Technical Center
Subject/TRT Terms:
Publication/ Report Number:

DOT/FAA/CT-87/26
Resource Type:

Tech Report
Geographical Coverage:

United States
Edition:

Final Report
Corporate Publisher:

United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center
Abstract:

This report presents the results of longitudinally impact testing a 10-foot section of a transport airplane at peak acceleration and corresponding velocity changas of 7.4g (22.4 ft/sec) and 14.2g (36 ft/sec), respectively. The purpose of the tests was to measure the responses of the fuselage and floor structure to simulated dynamic crash loads. The airframe test section included a full complement of seats and dummies. Acceleration and load/deflection response measurements were obtained from the instrumented fuselage, floor and seat/dummy installation.
Format:

PDF
Funding:

DTFA03-87-C-00013
Download URL:

https://rosap.ntl.bts.gov/view/dot/92923/dot_92923_DS1.pdf
File Type:

[PDF - 17.95 MB]
Collection(s):

FAA William J. Hughes Technical Center for Advanced Aerospace
Main Document Checksum:

urn:sha-512:77e09623f69f9e35f0bf5583348bce465a32cf6b2a865a3950b004193744ccd649073c265657cf9ccbdbf243b4774b6b7f31b37b0d3fe918e53b977d202ccbea

File Language:

English

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