Zobrazeno 1 - 10
of 25
pro vyhledávání: '"Raymond S. Castner"'
Publikováno v:
AIAA Scitech 2020 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::476e5684e42a9891e8c23e8990ee670c
https://doi.org/10.2514/6.2020-0003
https://doi.org/10.2514/6.2020-0003
Publikováno v:
25th AIAA/CEAS Aeroacoustics Conference.
An experimental study is conducted assessing the performance of an ejector together with an 8:1 aspect ratio rectangular nozzle with the eventual goal of noise reduction for jet engines. Wall static pressure and Pitot probe surveys are conducted to e
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a4551e6e408bd3bf44e09e02356b3fbb
https://doi.org/10.2514/6.2019-2494
https://doi.org/10.2514/6.2019-2494
Publikováno v:
AIAA Scitech 2019 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6ec20e36e47412eebca83dc37ff8d843
https://doi.org/10.2514/6.2019-0544
https://doi.org/10.2514/6.2019-0544
Publikováno v:
2018 Applied Aerodynamics Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5b612d921bded3f238ba5796b418700b
https://doi.org/10.2514/6.2018-2850
https://doi.org/10.2514/6.2018-2850
Publikováno v:
2018 Fluid Dynamics Conference.
Reynolds Averaged Navier-Stokes (RANS) simulations were performed on a Lockheed Martin Quiet SuperSonic Technology (QueSST) aircraft preliminary design to assess inlet performance. The FUN3D flow solver and its adjoint-based grid refinement capabilit
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d638ebdcf1116f3181d85827cad1b7e1
https://doi.org/10.2514/6.2018-3861
https://doi.org/10.2514/6.2018-3861
Autor:
Susan E. Cliff, Derek J. Dalle, Marie Denison, Nathanial T. Smith, Courtney S. Winski, Donald A. Durston, Brennan T. Blumenthal, Raymond S. Castner, Alaa A. Elmiligui, Melissa B. Carter, Patrick R. Shea
Publikováno v:
55th AIAA Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d93d7d93f01b69bf6f32f62d1e8db54d
https://doi.org/10.2514/6.2017-0041
https://doi.org/10.2514/6.2017-0041
Publikováno v:
58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
In late 2015, NASA's Aeronautics Research Mission Directorate (ARMD) funded an experiment in rapid design and rapid teaming to explore new approaches to solving challenging design problems in aeronautics in an effort to cultivate and foster innovatio
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2b30b9416dda40e70a5f00e958b4d104
https://doi.org/10.2514/6.2017-0976
https://doi.org/10.2514/6.2017-0976
Autor:
Walter E. Bruce, Melissa B. Carter, Alaa A. Elmiligui, Courtney S. Winski, Sudheer Nayani, Raymond S. Castner
Publikováno v:
54th AIAA Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::86744eb0775415b59c71433e6725b968
https://doi.org/10.2514/6.2016-2034
https://doi.org/10.2514/6.2016-2034
Autor:
Raymond S. Castner
Publikováno v:
Journal of Aircraft. 49:415-422
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::825530bc9adcc5a5794d3c6c1d50ef4d
https://doi.org/10.2514/1.c031305
https://doi.org/10.2514/1.c031305
Autor:
Raymond S. Castner
Publikováno v:
33rd AIAA Applied Aerodynamics Conference.
A plume and shock interaction study was developed to collect data and perform CFD on a configuration where a nozzle plume passed through the shock generated from the wing or tail of a supersonic vehicle. The wing or tail was simulated with a wedge-sh
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b6523055a374f1d29e3b3993c40b3ca6
https://doi.org/10.2514/6.2015-2263
https://doi.org/10.2514/6.2015-2263