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SAE ARP5905

Current

Current

The latest, up-to-date edition.

Calibration and Acceptance of Icing Wind Tunnels

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

26-09-2015

€170.13
Excluding VAT

1. SCOPE
2. APPLICABLE DOCUMENTS
3. SYMBOLS
4. FACILITY DESCRIPTION
5. FACILITY PERFORMANCE TARGETS
6. INSTRUMENTATION
7. FACILITY CALIBRATION
8. CALIBRATION PROCEDURES
9. ACCEPTANCE CRITERIA
10. CALIBRATION AND ACCEPTANCE REPORT
11. NOTES
APPENDIX A - LIQUID WATER CONTENT MEASUREMENT METHODS
APPENDIX B - WATER QUALITY, DROPLET FREEZE-OUT, AND
             DROPLET SUPERCOOLING
APPENDIX C - GUIDELINE TO DETERMINING DERIVED AERODYNAMIC
             PARAMETERS
APPENDIX D - EXAMPLE OF A FACILITY LIQUID WATER CONTENT
             CALIBRATION
APPENDIX E - NOZZLE WATER FLOW CALIBRATION PROCEDURE

Gives recommended practices for the calibration and acceptance of icing wind tunnels to be used in testing of aircraft components and systems and for the development of simulated ice shapes.

DocumentType
Standard
Pages
76
PublisherName
SAE International
Status
Current
Supersedes

This SAE Aerospace Recommended Practice (ARP) document provides recommended practices for the calibration and acceptance of icing wind tunnels to be used in testing of aircraft components and systems and for the development of simulated ice shapes. This document is not applicable to air-breathing propulsion test facilities configured for the purposes of engine icing tests. Use of facilities as part of an aircraft’s ice protection Certification Plan should be reviewed and accepted by the applicable regulatory agency prior to testing. Following acceptance of a test plan, data generated in these facilities may be submitted to regulatory agencies for use in the certification of aircraft ice protection systems and components. Certain types of tests may be appropriate in facilities with capabilities that are not as rigorously characterized as by the practices defined herein, and the acceptability of these tests should be coordinated with the applicable regulatory agency.

SAE AS 5562 : 2015 ICE AND RAIN MINIMUM QUALIFICATION STANDARDS FOR PITOT AND PITOT-STATIC PROBES
SAE AIR1667A Rotor Blade Electrothermal Ice Protection Design Considerations
FAA AC 20-147 : 2014 TURBOJET, TURBOPROP, TURBOSHAFT, AND TURBOFAN ENGINE INDUCTION SYSTEM ICING AND ICE INGESTION
SAE AIR 6189 : 2017 DESIGN, CALIBRATION, AND TEST METHODS FOR TURBINE ENGINE ICING TEST FACILITIES
SAE ARP5903 Droplet Impingement and Ice Accretion Computer Codes
FAA AC 23-16 : 0 POWERPLANT GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES AND AIRSHIPS
SAE ARP 5904 : 2002(R2012) AIRBORNE ICING TANKERS
FAA AC 25-28 : 2014 COMPLIANCE OF TRANSPORT CATEGORY AIRPLANES WITH CERTIFICATION REQUIREMENTS FOR FLIGHT IN ICING CONDITIONS
SAE AS 5498 : 2017 MINIMUM OPERATIONAL PERFORMANCE SPECIFICATION FOR INFLIGHT ICING DETECTION SYSTEMS
FAA AC 20-73 : 2006 AIRCRAFT ICE PROTECTION

FAA AC 25.1419-1 : 0 CERTIFICATION OF TRANSPORT CATEGORY AIRPLANES FOR FLIGHT IN ICING CONDITIONS
FAA AC 20-73 : 2006 AIRCRAFT ICE PROTECTION
SAE AIR 5504 : 2002 AIRCRAFT INFLIGHT ICING TERMINOLOGY
FAA AC 23.1419-2A : 0 CERTIFICATION OF PART 23 AIRPLANES FOR FLIGHT IN ICING CONDITIONS
SAE AIR5320A SUMMARY OF ICING SIMULATION TEST FACILITIES
AIAA S 071 : A1999 ASSESSMENT OF EXPERIMENTAL UNCERTAINTY WITH APPLICATION TO WIND TUNNEL TESTING
FAA AC 29-2 : 2008 CERTIFICATION OF TRANSPORT CATEGORY ROTORCRAFT
SAE ARP 5904 : 2002(R2012) AIRBORNE ICING TANKERS
SAE AIR 4906 : 2013 DROPLET SIZING INSTRUMENTATION USED IN ICING FACILITIES

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