Zobrazeno 1 - 10
of 25
pro vyhledávání: '"Catherine B. McGinley"'
Autor:
Mehdi R. Khorrami, Luther N. Jenkins, Catherine B. McGinley, Meelan M. Choudhari, David P. Lockard
Publikováno v:
AIAA Journal. 45:1930-1941
The current effort characterizes the details of flow interactions and wake interference effects between two cylinders in a tandem configuration. This setup is representative of several component-level flow interactions that occur when air flows over
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::54ae7eeccf54057eae302b1ee35a049f
https://doi.org/10.2514/1.23690
https://doi.org/10.2514/1.23690
Publikováno v:
Journal of Aircraft. 36:550-562
The confluent boundary layers over a three-element high-lift airfoil are studied using both numerical and experimental approaches. The results suggest that wake prediction is crucial to the convergence and accuracy of the overall solution. At maximum
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::307dee7a83028e7656433725fb2967ec
https://doi.org/10.2514/2.2490
https://doi.org/10.2514/2.2490
Publikováno v:
Experimental Thermal and Fluid Science. 13:21-28
A robust microsensor hot-film probe has been developed to obtain continuous turbulence measurements in moderately severe hypersonic environments. This probe represents a significant advancement of an existing concept. Optimization for hypersonic flow
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1875022b115d22479066f2149936610a
https://doi.org/10.1016/0894-1777(96)00001-5
https://doi.org/10.1016/0894-1777(96)00001-5
Autor:
William A. Wood, Catherine B. McGinley, Scott A. Berry, Rudolph A. King, Karen T. Berger, Michael A. Kegerise, Brian Anderson
Publikováno v:
48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition.
Updates to an analytic tool developed for Shuttle support to predict the onset of boundary layer transition resulting from thermal protection system damage or repair are presented. The boundary layer transition tool is part of a suite of tools that a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2fb342a4b4c58b8d928feedd2535ac98
https://doi.org/10.2514/6.2010-246
https://doi.org/10.2514/6.2010-246
Autor:
Benjamin S. Kirk, Kuo C. Wang, maria Barnell, Catherine B. McGinley, Gerald R. Kinder, Scott A. Berry
Publikováno v:
9th AIAA/ASME Joint Thermophysics and Heat Transfer Conference.
In support of the Shuttle Return to Flight program, a tool was developed to predict when boundary layer transition would occur on the lower surface of the orbiter during reentry due to the presence of protuberances and cavities in the thermal protect
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::81563eeff0a23cbf831c7fc2e6ab96b5
https://doi.org/10.2514/6.2006-2921
https://doi.org/10.2514/6.2006-2921
Autor:
P Lockard David, Catherine B. McGinley, Luther N. Jenkins, Medi R. Khorrami, Meelan M. Choudhari, Dan H. Neuhart
Publikováno v:
36th AIAA Fluid Dynamics Conference and Exhibit.
The current study is a continuation of our effort to characterize the details of flow interaction between two cylinders in a tandem configuration. This configuration is viewed to possess many of the pertinent flow features of the highly interactive u
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b41be22c3847ff90ac48ec1c262e3a66
https://doi.org/10.2514/6.2006-3203
https://doi.org/10.2514/6.2006-3203
Publikováno v:
35th AIAA Fluid Dynamics Conference and Exhibit.
§An analysis of the flow state on a trapezoidal wing model from the NASA 3-D High Lift Flow Physics Experiment is presented. The objective of the experiment was to characterize the flow over a non-proprietary semi-span three-element high-lift config
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b3d11f62bba0be5da880eb327bfb642e
https://doi.org/10.2514/6.2005-5148
https://doi.org/10.2514/6.2005-5148
Publikováno v:
11th AIAA/CEAS Aeroacoustics Conference.
Synergistic application of experiments and numerical simulations is crucial to understanding the underlying physics of airframe noise sources. The current effort is aimed at characterizing the details of the flow interaction between two cylinders in
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bf3bb75af082bcab0d42a04636574d36
https://doi.org/10.2514/6.2005-2866
https://doi.org/10.2514/6.2005-2866
Publikováno v:
11th AIAA/CEAS Aeroacoustics Conference.
A joint computational and experimental study has been performed at NASA Langley Research Center to investigate the unsteady flow generated by the components of an aircraft landing gear system. Because the flow field surrounding a full landing gear is
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ea5239d2e84aba86d659d44c3a22c545
https://doi.org/10.2514/6.2005-2812
https://doi.org/10.2514/6.2005-2812
Publikováno v:
24th AIAA Aerodynamic Measurement Technology and Ground Testing Conference.
This paper reviews existing microelectromechanical systems (MEMS)-based shear stress sensors. The promise and progress of MEMS scaling advantages to improve the spatial and temporal resolution and accuracy of shear stress measurement is critically re
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::934066e21522c1ef8958777da46abd6f
https://doi.org/10.2514/6.2004-2606
https://doi.org/10.2514/6.2004-2606