Aerodynamic load -- Measurement
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The concept Aerodynamic load -- Measurement represents the subject, aboutness, idea or notion of resources found in University of Missouri-St. Louis Libraries.
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Aerodynamic load -- Measurement
Resource Information
The concept Aerodynamic load -- Measurement represents the subject, aboutness, idea or notion of resources found in University of Missouri-St. Louis Libraries.
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- Aerodynamic load -- Measurement
9 Items that share the Concept Aerodynamic load -- Measurement
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- Wind tunnel tests of parabolic trough solar collectors, March 2001- August 2003
- A study of sampling rate requirements for load parameter statistics : final report
- Detailed pressure distribution measurements obtained on several configurations of an aspect-ratio-7 variable twist wing
- Final report : IEA Wind Annex XX : HAWT aerodynamics and models from wind tunnel measurements
- Fluctuating pressures measured beneath a high-temperature, turbulent boundary layer on a flat plate at a Mach number of 5
- In-flight investigation of shuttle tile pressure orifice installations
- Mean and peak wind load reduction on heliostats
- Measured pressure distributions inside nonaxisymmetric nozzles with partially deployed thrust reversers
- Strain gauge utilization for aerial vehicle dynamic load measurement
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<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.umsl.edu/resource/obPvkBbwPzk/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.umsl.edu/resource/obPvkBbwPzk/">Aerodynamic load -- Measurement</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.umsl.edu/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.umsl.edu/">University of Missouri-St. Louis Libraries</a></span></span></span></span></div>
