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
Mark Barnett
Published
1993 by National Aeronautics and Space Administration, National Technical Information Service, distributor in [Washington, DC], [Springfield, Va .
Written in English
Edition Notes
| 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 | |
|---|---|
| Format | Microform |
| Pagination | 1 v. |
| ID Numbers | |
| Open Library | OL14707409M |
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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.
