SAE ARP5905
Current
The latest, up-to-date edition.
Calibration and Acceptance of Icing Wind Tunnels
Hardcopy , PDF
English
26-09-2015
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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