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SAE ARP5765A

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by

Analytical Methods for Aircraft Seat Design and Evaluation

Available format(s)

Hardcopy , PDF

Superseded date

06-04-2021

Superseded by

SAE ARP5765B

Language(s)

English

Published date

04-12-2015

€175.52
Excluding VAT

1. SCOPE
2. REFERENCES
3. VIRTUAL ANTHROPOMORPHIC TEST DEVICE
   (V-ATD) CALIBRATION
4. SEAT SYSTEM VERIFICATION AND VALIDATION
5. MODEL USE
6. DOCUMENTATION OF V&V AND MODEL USE
7. BEST PRACTICES FOR TESTING AND MODELING
8. NOTES
APPENDIX A - METHODOLOGY FOR THE COMPARISON OF
             TEST AND SIMULATION WAVEFORMS
APPENDIX B - NIAR DATA SET FOR THE HYBRID 2 ATD
APPENDIX C - NIAR DATA SET FOR THE FAA HYBRID 3 ATD
APPENDIX D - SAMPLE HYBRID 2 V-ATD CALIBRATION REPORT
APPENDIX E - SYSTEM V&V EXAMPLES

Describes a means of assessing the credibility of computer models of aircraft seating systems used to simulate dynamic impact conditions set forth in Federal Regulations 14 CFR Part 23.562, 25.562, 27.562, and 29.562.

DocumentType
Standard
Pages
99
PublisherName
SAE International
Status
Superseded
SupersededBy
Supersedes

This SAE Aerospace Recommended Practice (ARP) defines a means of assessing the credibility of computer models of aircraft seating systems used to simulate dynamic impact conditions set forth in Federal Regulations §14 CFR Part 23.562, 25.562, 27.562, and 29.562. The ARP is applicable to lumped mass and detailed finite element seat models. This includes specifications and performance criteria for aviation specific virtual anthropomorphic test devices (v-ATDs). A methodology to evaluate the degree of correlation between a seat model and dynamic impact tests is recommended. This ARP also provides testing and modeling best practices specific to support the implementation of analytical models of aircraft seat systems. Supporting information within this document includes procedures for the quantitative comparison of test and simulation results, as well as test reports for data generated to support the development of v-ATDs and a sample v-ATD calibration report.

ASTM D 3941 : 2014 : REDLINE Standard Test Method for Flash Point by the Equilibrium Method With a Closed-Cup Apparatus
SAE AS8049C Performance Standard for Seats in Civil Rotorcraft, Transport Aircraft, and General Aviation Aircraft
MMPDS 08 : 2013 METALLIC MATERIALS PROPERTIES DEVELOPMENT AND STANDARDIZATION (MMPDS) - COMPLETE SET INCLUDES 9 CHAPTERS
FAA AC 20-146 : 2003 METHODOLOGY FOR DYNAMIC SEAT CERTIFICATION BY ANALYSIS FOR USE IN PARTS 23, 25, 27, AND 29 AIRPLANES AND ROTORCRAFT
SAE J211/1_201403 Instrumentation for Impact Test - Part 1 - Electronic Instrumentation
FAA AC 25.562-1 : 2006 DYNAMIC EVALUATION OF SEAT RESTRAINT SYSTEMS AND OCCUPANT PROTECTION ON TRANSPORT AIRPLANES
SAE J211/2_201406 Instrumentation for Impact Test—Part 2: Photographic Instrumentation
CFR 49(PTS572-999) : OCT 2017 TRANSPORTATION
ASTM E 8/E8M : 2016-09 TEST METHODS FOR TENSION TESTING OF METALLIC MATERIALS

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