Results 61 to 70 of about 162,037 (197)

Review of aerodynamic design in the Netherlands [PDF]

open access: yes
Aerodynamic design activities in the Netherlands, which take place mainly at Fokker, the National Aerospace Laboratory (NLR), and Delft University of Technology (TUD), are discussed.
Labrujere, Th. E.
core   +1 more source

The development of aerodynamic uncertainties for the space shuttle orbiter [PDF]

open access: yes, 1983
The Shuttle Program development schedule and the management decision to perform an orbital, manned mission on the first launch resulted in a requirement to develop realistic aerodynamic uncertainties for the preflight aerodynamic predictions.
Underwood, J. M., Young, J. C.
core   +1 more source

The aerodynamic design of an advanced rotor airfoil [PDF]

open access: yes
An advanced rotor airfoil, designed utilizing supercritical airfoil technology and advanced design and analysis methodology is described. The airfoil was designed subject to stringent aerodynamic design criteria for improving the performance over the ...
Blackwell, J. A., Jr., Hinson, B. L.
core   +1 more source

A New Cokriging Method for Variable-Fidelity Surrogate Modeling of Aerodynamic Data [PDF]

open access: yes, 2010
Cokriging is a statistical interpolation method for the enhanced prediction of a less intensively sampled primary variable of interest with assistance of intensively sampled auxiliary variables. In the geostatistics community it is referred to as two- or
Görtz, Stefan   +2 more
core   +1 more source

Experimental investigation on the optical emission spectroscopy of dielectric barrier discharge plasma actuators at different atmospheric pressures

open access: yesAIP Advances, 2018
The experiment of dielectric barrier discharge (DBD) plasma actuator using an asymmetrical electrodes configuration is conducted to investigate optical emission spectroscopy of the plasma discharge at pressures from 0.02 to 0.1 Mpa in air mixed with ...
S. Y. Xu, L. Kang, J. S. Cai, S. J. Tang
doaj   +1 more source

Comparison of testing results of three poorly streamlined entertainment venues / Trijų sudėtingo pavidalo pramoginių statinių maketų bandymų rezultatų gretinimas

open access: yesJournal of Civil Engineering and Management, 2012
The article discusses experimental investigations of wind effects and use of design codes for solving aerodynamic problems. It provides data regarding wind-tunnel tests conducted on three buildings with poorly streamlined shapes, including: methodology ...
Roman M. Pavlovsky   +3 more
doaj   +1 more source

Aerodynamic design using numerical optimization [PDF]

open access: yes
The procedure of using numerical optimization methods coupled with computational fluid dynamic (CFD) codes for the development of an aerodynamic design is examined.
Chapman, G. T., Murman, E. M.
core   +1 more source

Simulation of Unsteady Aerdynamic Load for Rigid Coaxial Rotor in Forward Flight with Vortex Particle Method [PDF]

open access: yes, 2017
Co-axial rotor systems are frequently used for high-speed helicopters. Nevertheless, issues related to rotor-head drag, aerodynamic performance and vibration should also be considered. Simulating the unsteady aerodynamic loads for a rigid coaxial rotor,
Barakos, George N.   +2 more
core  

Design, fabrication, and test of a composite material wind turbine rotor blade [PDF]

open access: yes
The aerodynamic design, structural design, fabrication, and structural testing is described for a 60 foot long filament wound, fiberglass/epoxy resin matrix wind turbine rotor blade for a 125 foot diameter, 100 kW wind energy conversion system. One blade
Griffee, D. G., Jr.   +2 more
core   +1 more source

The aerodynamic challenges of the design and development of the space shuttle orbiter [PDF]

open access: yes
The major aerodynamic design challenge at the beginning of the United States Space Transportation System (STS) research and development phase was to design a vehicle that would fly as a spacecraft during early entry and as an aircraft during the final ...
Gamble, J. D.   +9 more
core   +1 more source

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