Wind-Tunnel Balance Calibration with Temperature Using Design of Experiments-Reference-Cited by-同舟云学术

Wind-Tunnel Balance Calibration with Temperature Using Design of Experiments

Published:2014-05 Issue:3 Volume:51 Page:841-848
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Landman Drew¹,Yoder David²

Affiliation:

1. Department of Mechanical and Aerospace Engineering, Old Dominion University, Norfolk, Virginia 23529

2. IT&E/Flight Systems, Arnold Engineering Development Complex, U.S. Air Force and Aerospace Testing Alliance, Arnold Air Force Base, Tennessee 37389

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C032416

Reference9 articles.

1. Adapting second-order response surface designs to specific needs

2. Calibrating Large Capacity Aerodynamic Force Balance Instrumentation Using Response Surface Methods

3. “Recommended Practice: Calibration and Use of Internal Strain-Gage Balances with Application to Wind Tunnel Testing,” AIAA Rept. R-091-2003, AIAA, Reston, VA, 2003.

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