Zobrazeno 1 - 10
of 13
pro vyhledávání: '"Floyd J. Wilcox"'
Publikováno v:
54th AIAA Aerospace Sciences Meeting.
A wind-tunnel investigation of a 0.009 scale model of the Space Launch System (SLS) was conducted in the NASA Langley Unitary Plan Wind Tunnel to characterize the aerodynamics of the core and solid rocket boosters (SRBs) during booster separation. Hi
Autor:
Jeremy T. Pinier, Reynaldo J. Gomez, Floyd J. Wilcox, Stuart E. Rogers, Derek J. Dalle, David T. Chan
Publikováno v:
54th AIAA Aerospace Sciences Meeting.
The development of the aerodynamic database for the Space Launch System (SLS) booster separation environment has presented many challenges because of the complex physics of the ow around three independent bodies due to proximity e ects and jet inter-
Autor:
Linda S. Bangert, Marian Nemec, Floyd J. Wilcox, Alaa A. Elmiligui, Edward B. Parlette, Susan E. Cliff, Michael J. Aftosmis
Publikováno v:
29th AIAA Applied Aerodynamics Conference.
Accurate analysis of sonic boom pressure signatures using computational fluid dynamics techniques remains quite challenging. Although CFD shows accurate predictions of flow around complex configurations, generating grids that can resolve the sonic bo
Publikováno v:
29th AIAA Applied Aerodynamics Conference.
1 Aero/Performance Specialist, Supersonic Technology Development, P.O. Box 2206 M/S R-07, AIAA Associate Fellow. 2 Applied Aerodynamics, Supersonic Technology Development, P.O. Box 2206 M/S R-07, AIAA Senior Member 3 Applied Aerodynamics Technical Fe
Autor:
Floyd J. Wilcox, Gary E. Erickson
Publikováno v:
49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
Small-scale force and moment and pressure models based on the outer mold lines of the Ares I design analysis cycle crew launch vehicle were tested in the NASA Langley Research Center Unitary Plan Wind Tunnel from May 2006 to September 2009. The test
Publikováno v:
22nd Applied Aerodynamics Conference and Exhibit.
A wind-tunnel investigation of a square cross-section missile configuration has been conducted to obtain force and moment measurements, surface pressure measurements, and vapor screen flow visualization photographs for comparison with computational f
Publikováno v:
18th Applied Aerodynamics Conference.
This paper describes a series of wind tunnel experiments carried out with the aim of providing data suitable for evaluating the performance of Computational Fluid Dynamics (CFD) codes. The configurations and flow conditions studied are most relevant
Publikováno v:
Fluids 2000 Conference and Exhibit.
A review of the research conducted at the National Aeronautics and Space Administration (NASA), Langley Research Center (LaRC) into high-speed vortex flows during the 1970s, 1980s, and 1990s is presented. The data reviewed is for flat plates, cavitie
Autor:
Floyd J. Wilcox
Publikováno v:
Flow Visualization VI ISBN: 9783642848261
A surface flow visualization technique was developed that uses colored water as a medium to visualize surface flows over wind tunnel models at supersonic speeds. Wind tunnel tests were conducted with this technique used to visualize surface flows in
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4f4efb10b8fdd93fd0769c4ecd15d3b0
https://doi.org/10.1007/978-3-642-84824-7_4
https://doi.org/10.1007/978-3-642-84824-7_4
Autor:
Floyd J. Wilcox
Publikováno v:
29th Aerospace Sciences Meeting.
This paper presents a general overview of experimental research conducted in the area of tangential, semisubmerged, and internal store carriage and separation at supersonic speeds. Some of the advantages and disadvantages of tangential and semisubmer