Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Jeremy L. Hanke"'
Autor:
Noah M. Favaregh, Bandu N. Pamadi, Jing Pei, Peter F. Covell, Clyde R. Gumbert, Jeremy L. Hanke
Publikováno v:
Journal of Spacecraft and Rockets. 49:586-595
NASA Langley Research Center, in partnership with NASA Marshall Space Flight Center and NASA Ames Research Center, was involved in the aerodynamic analysis, testing, and database development for the Ares I A106 crew launch vehicle in support of the A
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ce8ba4f03ad37cb89640ae866d69bcb1
https://doi.org/10.2514/1.a32246
https://doi.org/10.2514/1.a32246
Autor:
Jeremy L. Hanke
Publikováno v:
Journal of Spacecraft and Rockets. 49:632-643
DOI: 10.2514/1.A32190 DuringthedevelopmentoftheAresIcrewlaunchvehicle,awind-tunnelmechanicalfailuredelayeddeliveryofthe ascent aerodynamics database for supersonic Mach numbers. An interim database developed from computational simulations mitigated t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ccf5ffddea90a16ce06eeb6e0e0120b6
https://doi.org/10.2514/1.a32190
https://doi.org/10.2514/1.a32190
Publikováno v:
52nd Aerospace Sciences Meeting.
Numerical simulations of the DLR-F11 wing/body high-lift configuration using the finitevolume-based solver STAR-CCM+ were performed based on the guidelines provided for the 2 AIAA CFD High Lift Prediction Workshop (HiLiftPW-2). Unstructured polyhedra
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e0a85a733c5792f15a1bd42eeb572457
https://doi.org/10.2514/6.2014-0914
https://doi.org/10.2514/6.2014-0914
Autor:
Karen L. Bibb, Jeremy L. Hanke, Michael J. Hemsch, David T. Chan, Eric L. Walker, Jeremy T. Pinier
Publikováno v:
29th AIAA Applied Aerodynamics Conference.
The NASA Constellation Program has worked for the past five years to develop a re- placement for the current Space Transportation System. Of the elements that form the Constellation Program, only two require databases that define aerodynamic environm
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6d8b70274f9f4a08e409ad54c96e9f45
https://doi.org/10.2514/6.2011-3345
https://doi.org/10.2514/6.2011-3345
Autor:
Jeremy L. Hanke
Publikováno v:
29th AIAA Applied Aerodynamics Conference.
The Ares I A106 Liftoff/Transition Force and Moment Aerodynamics Database describes the aerodynamics of the Ares I Crew Launch Vehicle (CLV) from the moment of liftoff through the transition from high to low total angles of attack at low subsonic Mac
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::20bb97927b328ef9f3f19633d0b1f659
https://doi.org/10.2514/6.2011-3647
https://doi.org/10.2514/6.2011-3647
Autor:
Jeremy L. Hanke
Publikováno v:
29th AIAA Applied Aerodynamics Conference.
The Ascent Force and Moment Aerodynamic (AFMA) Databases (DBs) for the Ares I Crew Launch Vehicle (CLV) were typically based on wind tunnel (WT) data, with increments provided by computational fluid dynamics (CFD) simulations for aspects of the vehic
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b5b3740a50cf7f6b5eef3db4788b528c
https://doi.org/10.2514/6.2011-3648
https://doi.org/10.2514/6.2011-3648
Autor:
Noah M. Favaregh, Bandu N. Pamadi, Clyde R. Gumbert, Jeremy L. Hanke, Jing Pei, Peter F. Covell
Publikováno v:
49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
NASA Langley Research Center, in partnership with NASA Marshall Space Flight Center and NASA Ames Research Center, was involved in the aerodynamic analyses, testing, and database development for the Ares I A106 crew launch vehicle in support of the A
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e325ddce4268fcc8eab9cd74283bffba
https://doi.org/10.2514/6.2011-12
https://doi.org/10.2514/6.2011-12
Publikováno v:
49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
The Ares I vehicle architecture was the design outcome of the Exploration Systems Architecture Study (ESAS) in response to the Vision For Space Exploration challenge provided by President George Bush in 2004. The Ares I vehicle was designed to carry
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9b5054cdbe652426877e9ea52a929896
https://doi.org/10.2514/6.2011-13
https://doi.org/10.2514/6.2011-13
Publikováno v:
26th AIAA Aerodynamic Measurement Technology and Ground Testing Conference.
A detailed uncertainty analysis for the Ares I ascent aero 6-DOF wind tunnel database is described. While the database itself is determined using only the test results for the latest configuration, the data used for the uncertainty analysis comes fro
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8a4eb081bbf9ce497c3490cf5b148834
https://doi.org/10.2514/6.2008-4259
https://doi.org/10.2514/6.2008-4259