The wind tunnel gives accurate results and is suitable for undergraduate study and research projects. TecQuipment offers a comprehensive range of optional models and instrumentation, including a computer-based data acquisition system. AF100 Features Saves time and money compared to full-scale wind-tunnels or airborne laboratories Operates at. Transonic tunnel. High subsonic wind tunnels (0.4 wind tunnels (0.75 subsonic wind tunnels. The highest speed is reached in the test section. The Mach number is approximately 1 with combined subsonic.
The complete starter set includes TecQuipment’s Subsonic Wind Tunnel (AF1300), the Basic Lift and Drag Balance (AF1300Z) and the Three-dimensional Drag Models (AF1300J) - all parts needed for experiments in aerodynamic drag. SUBSONIC WIND TUNNEL AF100/TECQ A compact, practical open-circuit suction wind tunnel for studying aerodynamics. The wind tunnel saves time and money compared with full-scale wind tunnels or airborne laboratories, and it offers a wide variety of experiments.
These are the sources and citations used to research Stress Concentration. This bibliography was generated on Cite This For Me on
Subsonic Wind Tunnel Experiment
AF100 subsonic wind tunnel user guide
2015 - Tecequipment
In-text: (AF100 subsonic wind tunnel user guide, 2015)Your Bibliography: AF100 subsonic wind tunnel user guide. (2015). Tecequipment, p.3.Budynas, R.
Shigley's mechanical engineering design
2013 - Mcgraw-Hill Education
In-text: (Budynas, 2013)Your Bibliography: Budynas, R. (2013). Shigley's mechanical engineering design. Mcgraw-Hill Education, pp.1026-1027.NI 9923 - Dimensional Drawing - National Instruments
2018
In-text: (Digital.ni.com, 2018)Your Bibliography: Digital.ni.com. (2018). NI 9923 - Dimensional Drawing - National Instruments. [online] Available at: http://digital.ni.com/hardref.nsf/websearch/30C4F1E2538683F1862579BF00505774?OpenDocument&node=132120_US [Accessed 26 Apr. 2018].Osborne Reynolds
2018
In-text: (En.wikipedia.org, 2018)Your Bibliography: En.wikipedia.org. (2018). Osborne Reynolds. [online] Available at: https://en.wikipedia.org/wiki/Osborne_Reynolds [Accessed 28 Mar. 2018].George, C.
Experimental Evaluation of Stress Concentration and Intensity Factors
2013 - Springer Verlag
In-text: (George, 2013)Your Bibliography: George, C. (2013). Experimental Evaluation of Stress Concentration and Intensity Factors. Springer Verlag.Gibson, L. and Andrews, E. W.
The influence of cracks, notches and holes on the tensile strength of cellular solids
2001 - Elsevier
In-text: (Gibson and Andrews, 2001)Your Bibliography: Gibson, L. and Andrews, E. (2001). The influence of cracks, notches and holes on the tensile strength of cellular solids. Elsevier.Boundary Layer
2018
In-text: (Grc.nasa.gov, 2018)Your Bibliography: Grc.nasa.gov. (2018). Boundary Layer. [online] Available at: https://www.grc.nasa.gov/www/k-12/airplane/boundlay.html [Accessed 28 Mar. 2018].Dynamics of Flight
2018
In-text: (Grc.nasa.gov, 2018)Your Bibliography: Grc.nasa.gov. (2018). Dynamics of Flight. [online] Available at: https://www.grc.nasa.gov/WWW/k-12/UEET/StudentSite/dynamicsofflight.html#wings [Accessed 23 Feb. 2018].Hearn, E. J.
Mechanics of materials
1997 - Butterworth-Heinemann - Oxford
In-text: (Hearn, 1997)Your Bibliography: Hearn, E. (1997). Mechanics of materials. Oxford: Butterworth-Heinemann.Anon
2018
In-text: (Me.utep.edu, 2018)Your Bibliography: Me.utep.edu. (2018). [online] Available at: http://me.utep.edu/cmstewart/documents/ME3334/Lecture%207%20-%20Supplemental.pdf [Accessed 28 Mar. 2018].Schetz, J. A. and Bowersox, R. D. W.
Boundary layer analysis
2012 - American Institute of Aeronautics and Astronautics - Reston, Va
In-text: (Schetz and Bowersox, 2012)Your Bibliography: Schetz, J. and Bowersox, R. (2012). Boundary layer analysis. Reston, Va: American Institute of Aeronautics and Astronautics.NI 9923 - National Instruments
2018
In-text: (Sine.ni.com, 2018)Your Bibliography: Sine.ni.com. (2018). NI 9923 - National Instruments. [online] Available at: http://sine.ni.com/nips/cds/view/p/lang/en/nid/210164 [Accessed 26 Apr. 2018].Young, W. C., Budynas, R. G. and Sadegh, A. M.
Roark's formulas for stress and strain
2012 - McGraw-Hill - London
In-text: (Young, Budynas and Sadegh, 2012)Your Bibliography: Young, W., Budynas, R. and Sadegh, A. (2012). Roark's formulas for stress and strain. London: McGraw-Hill.