Aerodynamics
Resource Information
The concept Aerodynamics represents the subject, aboutness, idea or notion of resources found in University of Missouri-St. Louis Libraries.
The Resource
Aerodynamics
Resource Information
The concept Aerodynamics represents the subject, aboutness, idea or notion of resources found in University of Missouri-St. Louis Libraries.
- Label
- Aerodynamics
- Authority link
- http://id.worldcat.org/fast/00798195
- Source
- fast
25 Items that share the Concept Aerodynamics
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Context of AerodynamicsSubject of
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- A direct-fire trajectory model for supersonic, transonic, and subsonic projectile flight
- Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0
- Aerodynamic design of transport aircraft
- Aircraft performance and sizing, Volume II, Applied aerodynamic design
- Atmospheric turbulence, meteorological modeling and aerodynamics
- CAST-10-2/DOA 2 Airfoil Studies Workshop results : proceedings of a workshop sponsored by the National Aeronautics and Space Administration and held at NASA Langley Research Center, Hampton, Virginia, September 23-27, 1988
- Composite materials and structures in aerospace engineering : selected plenary lectures and key-note contributions of the two events FULLCOMP -- Meeting FULLy integrated analysis, design, manufacturing and health-monitoring of COMPosite structures and 23rd Congress of AIDAA, Associazione Italiana di Aeronautica ed Astronautica November 17-21, 2015, Torino, Italy
- Dual methods and approximation concepts in structural synthesis
- Dynamic ground effect for a cranked arrow wing airplane
- Dynamic modeling of starting aerodynamics and stage matching in an axi-centrifugal compressor
- Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV
- Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements
- Flight dynamics principles
- Flight vehicle aerodynamics
- Hypersonic lateral and directional stability characteristics of aeroassist flight experiment configuration in air and CF4
- Leading-edge deflection optimization for a highly swept arrow-wing configuration
- Pressure distribution for the wing of the YAV-8B airplane ; with and without pylons
- Research engineering annual report
- Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8° to 90°
- STARS, an integrated, multidisciplinary, finite-element, structural, fluids, aeroelastic, and aeroservoelastic analysis computer program
- Subsonic flight test evaluation of a propulsion system parameter estimation process for the F-100 engine
- The Enigma of the Aerofoil : Rival Theories in Aerodynamics, 1909-1930
- The encyclopedia of aerodynamics
- Why don't jumbo jets flap their wings? : flying animals, flying machines, and how they are different
- Wing theory
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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/5xZ0Q-p7Ydo/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.umsl.edu/resource/5xZ0Q-p7Ydo/">Aerodynamics</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>