Published Papers
This page provides the following list of papers related to balance technologies. Please contact us if you would like to add a paper to this list.
This document provides a recommended method for calibration of internal strain-gage balances used in wind tunnel testing. The practices include terminology, axis system definition, balance calibration methods, matrix, and documentation. Use of this document will facilitate the exchange of information among users, suppliers, and other interested parties. List Price: $51.95
Papers Presented at AIAA Events
- Development of a New Flow-Through Force Measurement Balance with Improved Accuracy for use in Powered Wind Tunnel Model Testing
Andrew C. Roberts, NASA Ames Research Center, CA; Kenneth M. Smith, Microcraft Inc, Tullahoma, TN
AIAA 88-2059, May 1988
- A Single-Vector Force Calibration Method Featuring the Modern Design of Experiments (Invited)
P.A. Parker, M. Morton, N. Draper, W. Line, NASA Langley Research Center, VA
AIAA 2001-0170, January 2001
- Strain-Gage Balance Calibration Analysis Using Automatically Selected Math Models
N. Ulbrich and T. Volden, Sverdrup Technology, Inc., NASA Ames Research Center, Moffett Field, CA
AIAA 2005-4084, July 2005
- Application Of A New Calibration Analysis Process To The MK-III-C Balance
N. Ulbrich and T. Volden, Sverdrup Technology, Inc., NASA Ames Research Center, Moffett Field, CA
AIAA 2006-0517, January 2006
- Development of a New Software Tool for Balance Calibration Analysis
N. Ulbrich and T. Volden, Sverdrup Technology, Inc., NASA Ames Research Center, Moffett Field, CA
AIAA 2006-3434, May 2006
- Analysis of Floor Balance Calibration Data Using Automatically Generated Math Models
N. Ulbrich and T. Volden, Sverdrup Technology, Inc., NASA Ames Research Center, Moffett Field, CA
AIAA 2006-3437, May 2006
- Analysis of Balance Calibration Machine Data Using Automatically Generated Math Models
N. Ulbrich and T. Volden, Jacobs Technology Inc., Moffett Field, CA
AIAA 2007-0145, January 2007
- A Comparison of Two Balance Calibration Model Building Methods
Richard DeLoach, NASA Langley Research Center, VA; N. Ulbrich, Jacobs Technology Inc., Moffett Field, CA
AIAA 2007-0147, January 2007
- Load Envelope Analysis of Strain-Gage Balance Data
N. Ulbrich and T. Volden, Jacobs Technology Inc., Moffett Field, CA
AIAA 2007-0354, January 2007
- Regression Analysis of Experimental Data Using an Improved Math Model Search Algorithm
N. Ulbrich and T. Volden, Jacobs Technology Inc., Moffett Field, CA
AIAA 2008-833, January 2008
- Predictive Capabilities of Regression Models used for Strain-Gage Balance Calibration Analysis
N. Ulbrich and T. Volden, Jacobs Technology Inc., Moffett Field, CA
D. Booth, Triumph Aerospace, Force Measurement Systems, San Diego, CA
AIAA-2008-4028, June 2008
Strain Gauge Balance Paper presented at the ISA 46th International Instrumentation Symposium
Papers from Proceedings of the 2nd International Symposium on Strain-Gage-Balances
04-07 May 1999
Bedford, England, UK
Investigation of the integrity of tapered balance joints and their effect on lift/drag interactions and
rolling moment measurements R.D. Law
Defence Evaluation Research Agency
Bedford, UK
Aerodynamic Microbalance Calibration System
Yang Yanguang, Tang Zhigong
China Aerodynamics Research and Development Center
Mianyang, Sichuan, China
On the development of a thin shell fin balance
Peter M. Bedgood
Defencetek, CSIR
P.O. Box 395
Pretoria, South Africa
Rotating balances for direct propeller performance evaluation on motorised models
M. Bazin, J.F. Bret, T. Fetet, Marc Jacquemmoz
Onera, Grands Moyens Techniques
Facilities for Forces Measurement of Hypersonic Wind Tunnel Tests in BIA
Yu Tao, Lixin Liao, Yulin Li
Beijing Institute of Aerodynamics
Beijing 7215, 100074, People’s Republic of China
Balance Technique for jet models wind tunnel testing
V.I. Lagutin, V.I. Lapygin
Central Research Institute of Machine Building (TSNIIMASH)
Russia
The six-component balance for blunt models aerodynamic force measurement in shock tunnel
Lu Zhiquo, Liu Hongshan, Zhang Yan
China Aerodynamics Research and Development Center
Mianyang, Sichuan, China
Automatic Repositioning Calibration rig for strain gage balance
Wang Jinyin, Liu Shuwei, Chen Liangze
Beijing Institute of Aerodynamics
100074, P.O. Box 7201-12
Beijing, P.R. China
Capabilities of NASA Ames Research Center’s Automated balance calibration machine
Chris Lockwood, Sverdrup, NASA Ames Division
Phil Luan, Sverdrup, NASA Ames Division
Pat Whittaker, Wind Tunnel Systems Branch, NASA Ames Research Center, Moffett Field, CA 94035
A study of Automatic Balance Calibration System Capabilities
Peter A. Parker, Ray D. Rhew
NASA Langley Research Center
Hampton, Virginia, USA
Balance Calibration and Performance Comparisons using 6-component Loads Derived from Actual Wind Tunnel Test Data
Dennis Booth, Richard Crooks, Allen Zwan
Micro Craft Technology
San Diego, California
A Consideration of Tare Weight Effects in Calibration and Use of Wind Tunnel Strain-Gauge Balances
Robin D. Galway
RobGal Aerotest Consulting, Ottawa, Canada
The Wind Tunnel Balance as Part of a System
David G. Coulton
Head of Technology
Aircraft Research Association Ltd.
Manton Lane, Bedford, MK41 7PF, England
Determination of Bias and Precision Uncertainties of a Strain Gauge Balance by Replicated Machine Calibration
John S. Tripp, Ping Tcheng
NASA Langley Research Center
Hampton, Virginia, USA
A New Half-Model-Balance for the Cologne-Cryogenic-Wind-Tunnel (Kryo-Kanal Köln)
Dr.-Ing. Klaus Hufnagel
Dipl.-Ing. Rudiger Rebstock
Dr.-Ing. Junnai Zhai
Temperature Control of External Balances for Semi-Span Models in Cryogenic Tunnels
S. Balakrishna, ViGYAN Inc.,
W.A. Kilgore, Veridan Engineering
D.H. Butler, Veridan Engineering
The application of an automatic balance calibration machine to examine the effect of air feed systems on half model balances
R.D. Law
Defence Evaluation Research Agency, Bedford, UK
The fully automatic balance calibration system (FABCS-3T) and the uncertainty analysis
Ma Husheng, Zhang Yingpei, Yu Kunlong, Yang Qilin, Tian Hongsheng
China Aerodynamics Research and Development Center
Mianyang, Sichuan, P.R. of China
TIGER: Development of Thermal Gradient Compensation Algorithms and Techniques
James Herford, Christopher Newport University, Newport News, VA
Peter A. Parker, Ray D. Rhew
NASA Langley Research Center, Hampton, VA
Improvements in sting balance calibration techniques
Michael Levkovitch, Doron Tchechik
Engineering Division
Israel Aircraft Industries Ltd.
Measures for Control of Wind Tunnel Balance Load and Fatigue Life
Gustav Ingmar Johnson
The Aeronautical Research Institute of Sweden (FFA)
A strain gauge balance calibration system at the Aeronautical and Maritime Research Laboratory
Stephen S.W. Lan
Air Operations Division
Aeronautical and Maritime Research Laboratory
Defence Science and Technology Organisation
Melbourne, Australia
Predesign and Optimization of Half-Model-Balances for Cryogenic Wind Tunnels by Finite Element Analysis
Dipl.-Ing. Rudiger Rebstock (DLR)
Dr.-Ing. Junnai Zhai (DLR)
Dr.-Ing. Klaus Hufnagel (TUD)
The Planned AGARDograph of the Internal Balance Technology
Prof. Dipl.-Ing. Bernd F.R. Ewald
Darmstadt University of Technology, Germany