Zobrazeno 1 - 10
of 16
pro vyhledávání: '"Morris E. Childs"'
Autor:
Chen-Chih Sun, Morris E. Childs
Publikováno v:
AIAA Journal. 13:224-227
An analysis of turbulent boundary layer flow characteristics and the computational procedure used are discussed. The integrated mass and momentum flux profiles and differentials of the integral quantities are used in the computations so that local ev
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::23a2c748eaa3b5b1f0e34db1a4540ed6
https://doi.org/10.2514/3.49670
https://doi.org/10.2514/3.49670
Autor:
Morris E. Childs, Deepak Om
Publikováno v:
Journal of Propulsion and Power. 1:393-398
An approximate integral viscous-inviscid interaction method is presented for calculating the development of a turbulent boundary layer subjected to a normal shock wave in an internal flow. The inflow conditions and the downstream pressure are provide
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::006d92ea29d02278f5a027b14189fc89
https://doi.org/10.2514/3.22815
https://doi.org/10.2514/3.22815
Publikováno v:
AIAA Journal. 23:707-714
Detailed pitot, static, and wall pressure measurements have been obtained for a transonic normal shockwave/turbulent boundary-layer interaction at freestream Mach numbers of 1.28, 1.37, and 1.48, and at a constant unit Reynolds number of 4.92xl0 6/m
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a140983335ba784c3f58788312963e32
https://doi.org/10.2514/3.8974
https://doi.org/10.2514/3.8974
Autor:
Morris E. Childs, Deepak Om
Publikováno v:
AIAA Journal. 23:1506-1511
An experimental study is described in which detailed pitot, static, and wall pressure measurements have been obtained for multiple transonic shock-wave/turbulent boundary-layer interactions in a circular duct at a freestream Mach number of 1.49, a un
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ac4c3e26085ae125b536b5a703481014
https://doi.org/10.2514/3.9117
https://doi.org/10.2514/3.9117
Publikováno v:
Journal of Aircraft. 7:137-140
Compressible turbulent boundary layers velocity profiles, Coles universal wake function, least squares methods, wake-wall representation, etc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fb309c4f6be03216bf9b26f6a1d905b0
https://doi.org/10.2514/3.44136
https://doi.org/10.2514/3.44136
Autor:
Morris E. Childs, Chen-Chih Sun
Publikováno v:
Journal of Aircraft. 11:54-59
A computation procedure is described for predicting the flowfields which develop when successive interactions between oblique shock waves and a turbulent boundary layer occur. Such interactions may occur, for example, in engine inlets for supersonic
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a66da10af90b690dbcb433c996261e52
https://doi.org/10.2514/3.60321
https://doi.org/10.2514/3.60321
Publikováno v:
AIAA Journal. 2:312-321
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f6c3f07ea1b176fdcae474d59eca0f6d
https://doi.org/10.2514/3.2289
https://doi.org/10.2514/3.2289
Publikováno v:
Journal of Aircraft. 5:461-467
Methods for calculating the changes in turbulent boundary-layer characteristics across an oblique shock reflection based on integral flow models are developed for two-dimensional and axially symmetric flows with solid boundaries and mass bleed throug
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5c7e3a1cfafe8dd1bae4f4af2752f9b4
https://doi.org/10.2514/3.43967
https://doi.org/10.2514/3.43967
Autor:
Morris E. Childs, Chen-Chih Sun
Publikováno v:
AIAA Journal. 14:820-822
A form of the wall-wake profile, which is applicable to flows with heat transfer, and for which a variation in y = O at y = delta, was suggested. The modified profile, which takes into account the effect of turbulent Prandtl number, was found to prov
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::21c7e1c2e65a35298af32b889e242a27
https://doi.org/10.2514/3.7157
https://doi.org/10.2514/3.7157
Publikováno v:
AIAA Journal. 11:761-763
Additional incipient separation data presented cover a range of Reynolds numbers not covered in previous investigations conducted by Seebaugh (1968) and Rose (1972). A novel technique for detecting incipient separation is discussed. Several methods f
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::157613a4ccc41b820f6f30e924810509
https://doi.org/10.2514/3.6829
https://doi.org/10.2514/3.6829