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Experimental Design Considerations for Calibration of Semispan Force Measurement Systems

  • Published:2015-03 Issue:2 Volume:52 Page:638-649
  • ISSN:0021-8669
  • Container-title:Journal of Aircraft
  • language:en
  • Short-container-title:Journal of Aircraft

Author:

Lynn Keith C.1,Commo Sean A.1,Ulbrich Norbert M.2,Harris Colin P.3

Affiliation:

1. Aeronautics Systems Engineering Branch, NASA Langley Research Center, Hampton, Virginia 23681

2. Wind-Tunnel Division, Jacobs Technology, Inc., Moffett Field, California 94035

3. Triumph Aerospace, Force Measurement Systems, Triumph Group, Inc., San Diego, California 92121

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference16 articles.

1. High-Reynolds Number Active Blowing Semi-Span Force Measurement System Development

2. Development of the NTF-117S Semi-span Balance (Invited)

3. Calibration Variable Selection and Natural Zero Determination for Semispan and Canard Balances

4. MyersR. H.MontgomeryD. C., Response Surface Methodology, 2nd ed., Wiley, New York, 2002, pp. 303–429.

5. MyersR. H., Classical and Modern Regression with Applications, 2nd ed., Duxbury Press, Belmont, CA, 1990, pp. 82–153.

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