Wings
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The concept Wings represents the subject, aboutness, idea or notion of resources found in San Francisco Public Library.
The Resource
Wings
Resource Information
The concept Wings represents the subject, aboutness, idea or notion of resources found in San Francisco Public Library.
- Label
- Wings
- Source
- nasat
25 Items that share the Concept Wings
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- Wind tunnel results of the aerodynamic performance of a 1/8-scale model of a twin-engine transport with multi-element wing
- A numerical model of unsteady, subsonic aeroelastic behavior
- Aeroelastic deformation : adaptation of wind tunnel measurement concepts to full-scale vehicle flight testing
- Application of approximate unsteady aerodynamics for flutter analysis
- Computational icing risk analysis of the D8 "Double Bubble" aircraft
- Deformed shape calculation of a full-scale wing using fiber optic strain data from a ground loads test
- Design verification and fabrication of active control systems for the DAST ARW-2 high aspect ratio wing
- Evaluation of low noise integration concepts and propulsion technologies for future supersonic civil transports
- Experimental investigation of water droplet impingement on airfoils, finite wings, and an S-duct engine inlet
- Finite element analysis and test results comparison for the hybrid wing body center section test article
- Initiation of long-wave instability of vortex pairs at cruise altitudes
- Measuring global surface pressures on a circulation control concept using pressure sensitive paint
- Methods for in-flight wing shape predictions of highly flexible unmanned aerial vehicles : formulation of Ko displacement theory
- Nacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds
- Nonlinear aerodynamic wing design
- Numerical study of steady and unsteady canard-wing-body aerodynamics
- Numerical study of three-dimensional separation and flow control at a wing-body junction : progress report for the period ended April 30, 1989
- On approximate factorization schemes for solving the full potential equation
- Reduced uncertainties in the flutter analysis of the aerostructures test wing
- Reliability based design for a raked wing tip of an airframe
- Sensitivity of F-106B leading-edge-vortex images to flight and vapor-screen parameters
- Space shuttle pinhole formation mechanism studies
- Structural test documentation and results for the McDonnell Douglas all-composite wing stub box
- Structural testing of a stitched/resin film infused graphite-epoxy wing box
- Validation of design and analysis techniques of tailored composite structures
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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.sfpl.org/resource/w76hiGNa29E/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.sfpl.org/resource/w76hiGNa29E/">Wings</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.sfpl.org/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="https://link.sfpl.org/">San Francisco Public Library</a></span></span></span></span></div>
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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.sfpl.org/resource/w76hiGNa29E/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.sfpl.org/resource/w76hiGNa29E/">Wings</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.sfpl.org/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="https://link.sfpl.org/">San Francisco Public Library</a></span></span></span></span></div>
