3 edition of An analysis for high Reynolds number inviscid/viscid interactions in cascades found in the catalog.
An analysis for high Reynolds number inviscid/viscid interactions in cascades
1993 by National Aeronautics and Space Administration, National Technical Information Service, distributor in [Washington, DC], [Springfield, Va .
Written in English
|Statement||Mark Barnett, Joseph M. Verdon, and Timothy C. Ayer.|
|Series||[NASA contractor report] -- NASA CR-4519., NASA contractor report -- NASA CR-4519.|
|Contributions||Verdon, Joseph M., Ayer, Timothy C., United States. National Aeronautics and Space Administration.|
|The Physical Object|
Secondary school case studies
Hymns, composed by different authors, by order of the General Convention of Universalists of the New-England states and others
Coast Guard Authorization Act of 1984
A present ansvver to the late complaint unto the House of Commons. By divers members of the said House
The Pennsylvania, New-Jersey, Delaware, Maryland, and Virginia almanac, for the year of our Lord, 1805 ...
The radical center
Vegetarian Cooking for Beginners
Aquifer vulnerability analysis using the pesticide root-zone model (PRZM2)
Catholic art education: the new trends
The capns wife
Get this from a library. An analysis for high Reynolds number inviscid/viscid interactions in cascades. [Mark Barnett; Joseph M Verdon; Timothy C Ayer; United States. National Aeronautics and. American Institute of Aeronautics and Astronautics Sunrise Valley Drive, Suite Reston, VA Analysis of High Reynolds Number Inviscid/ Viscid Interactions in Cascades J Thrust Imparted to an Airfoil by Passage Through a Sinusoidal Upwash Field J Prismatic Grid Generation for Three-Dimension-al Complex Geometries J Observations of Liquid Jets Injected into a High-ly Accelerated Supersonic Boundary Layer JAn analysis for high Reynolds number inviscid/viscid interactions in cascades book of aerodynamics: bases of aerodynamic design / Arnold M.
Kuethe, Chuen-Yen Chow Wiley New York Wikipedia Citation Please see Wikipedia's template documentation for further citation fields that may be required. Abstract. A recently developed nonlinear, compressible viscous-layer analysis and code has been extended and coupled to a linearized inviscid aerodynamic analysis to predict high Reynolds number subsonic unsteady flows through isolated, two-dimensional blade by: 1.
This banner text can have markup. web; books; video; audio; software; images; Toggle navigation. Thus, high Reynolds number flows driven by small amplitude unsteady excitations have been considered. The resulting analyses should apply in many practical situations and lead to a better.
An efficient analysis for predicting steady, inviscid-viscid interaction phenomena, such as viscous-layer separation, shock/boundary-layer interaction, and trailing-edge/near-wake interaction, in. The leading-edge flaps were deflected 4 deg to 15 deg, and the trailing-edge flaps were deflected from deg to 10 deg.
Longitudinal force and moment data were obtained at Mach numbers of,and for an angle-of-attack range 4 deg to 20 deg at a Reynolds number of x 10(exp 6) per foot and for an angle-of-attack range 4.