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Performance Tests of Wire Strain Gages

Performance Tests of Wire Strain Gages PDF Author: William R. Campbell
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 606

Book Description
Results of calibrations to determine axial and transverse strain sensitivities are presented for 15 types of single-element, multistrand wire strain gage.

Performance Tests of Wire Strain Gages

Performance Tests of Wire Strain Gages PDF Author: William R. Campbell
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 606

Book Description
Results of calibrations to determine axial and transverse strain sensitivities are presented for 15 types of single-element, multistrand wire strain gage.

Tests of Six Types of Bakelite-bonded Wire Strain Gages

Tests of Six Types of Bakelite-bonded Wire Strain Gages PDF Author: William R. Campbell
Publisher:
ISBN:
Category : Strain gages
Languages : en
Pages : 690

Book Description
Tests were made to determine the important performance characteristics for six types of bakelite-bonded wire strain gages commercially available and in current use by the aircraft industry. Results on the following characteristics are presented: (1) uniformity of calibration factors for individual gages of the same type, (2) variation of calibration factor with temperature, (3) creep, (4) effect of current on gage resistance, and (5) variation of gage resistance with temperature.

Index of NACA Technical Publications

Index of NACA Technical Publications PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 616

Book Description


Technical Note - National Advisory Committee for Aeronautics

Technical Note - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 876

Book Description


Characteristics and Applications of Resistance Strain Gages

Characteristics and Applications of Resistance Strain Gages PDF Author: United States. National Bureau of Standards
Publisher:
ISBN:
Category : Strain gages
Languages : en
Pages : 150

Book Description


An Investigation of Aircraft Heaters

An Investigation of Aircraft Heaters PDF Author: Llewellyn Michael Kraus Boelter
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 666

Book Description
An analysis is presented of the factors determining the power efficiency of radiation thermopiles of that type in which the receivers consist either of parts of the conductors themselves or of coatings or other electrically insulating materials in intimate contact with these conductors. On the basis of this analysis, which is applicable to thermopiles of a wide variety of constructions and materials, criterions for maximum power efficiency can be calculated. Such criterions are obtained for a silver-constantan plated-type thermopile. The design and construction of thermopiles in accordance with these criterions are described, and test data are reported, showing agreement between actual and predicted performance.

Handbook of Supersonic Aerodynamics

Handbook of Supersonic Aerodynamics PDF Author: R. J. Volluz
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 512

Book Description


Handbook of Supersonic Aerodynamics

Handbook of Supersonic Aerodynamics PDF Author: Johns Hopkins University. Applied Physics Laboratory, Silver Spring, Md
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 516

Book Description


Technical Note

Technical Note PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388

Book Description


Measurement of the Arithmetic Mean Velocity of a Pulsating Flow of High Velocity by the Hot-wire Method

Measurement of the Arithmetic Mean Velocity of a Pulsating Flow of High Velocity by the Hot-wire Method PDF Author: John R. Weske
Publisher:
ISBN:
Category : Air flow
Languages : en
Pages : 642

Book Description
Through the addition of a nonlinear amplifier stage the reading of the instrument has been rendered proportional to the velocity.