Zobrazeno 1 - 10
of 19
pro vyhledávání: '"Stefanie M. Hirt"'
Autor:
Voytovych Dmytro Mykolayovych, David J. Arend, John D. Wolter, Sharma Om P, John A. Gazzaniga, William T. Cousins, Stefanie M. Hirt, Larry W. Hardin
Publikováno v:
Volume 2A: Turbomachinery.
An experimental investigation has been completed of the performance and operability of a first of its kind 0.289 scale boundary layer ingesting propulsor within the new 6.5ft × 6ft transonic embedded propulsor testbed of NASA’s 8ft × 6ft Superson
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2581acbab4f1886c2893f0831ffb8ca1
https://doi.org/10.1115/gt2020-15695
https://doi.org/10.1115/gt2020-15695
Publikováno v:
2018 AIAA Aerospace Sciences Meeting.
The design of a unique distortion-tolerant fan for a high-bypass ratio boundary-layer ingesting propulsion system has been completed and a rig constructed and tested in the NASA Glenn 8’x6’ wind tunnel. Processing the data from the experiment pre
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::27e16108fb59db5cc3f0181bab7cffce
https://doi.org/10.2514/6.2018-1888
https://doi.org/10.2514/6.2018-1888
Autor:
John D. Wolter, Tristan A. Hearn, John A. Gazzaniga, Stefanie M. Hirt, Larry W. Hardin, David J. Arend
Publikováno v:
2018 AIAA Aerospace Sciences Meeting.
A test of the Boundary Layer Ingesting-Inlet / Distortion-Tolerant Fan was completed in NASA Glenn's 8-Foot by 6-Foot supersonic wind tunnel. Inlet and fan performance were measured by surveys using a set of rotating rake arrays upstream and downstre
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8b624fc0da70032ff764400f40179957
https://doi.org/10.2514/6.2018-1889
https://doi.org/10.2514/6.2018-1889
Publikováno v:
53rd AIAA/SAE/ASEE Joint Propulsion Conference.
The recent Boundary-Layer-Ingesting Inlet/Distortion Tolerant Fan wind tunnel experiment at NASA Glenn Research Center's 8- by 6-foot Supersonic Wind Tunnel (SWT) examined the performance of a novel inlet and fan stage that was designed to ingest the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::54cdc083e8d78fee69f7f0fac544acdb
https://doi.org/10.2514/6.2017-4636
https://doi.org/10.2514/6.2017-4636
Publikováno v:
53rd AIAA/SAE/ASEE Joint Propulsion Conference.
In order to test embedded-propulsor technology, modifications were required of the 8x6 Supersonic Wind tunnel at NASA Glenn Research Center. The extent of the modifications required that a new tunnel calibration be completed to generate a new calibra
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a00de03415f9215aa82671926648e3e1
https://doi.org/10.2514/6.2017-5043
https://doi.org/10.2514/6.2017-5043
Autor:
William T. Cousins, Stefanie M. Hirt, John D. Wolter, Larry W. Hardin, Andrew J. Provenza, John A. Gazzaniga, Sharma Om P, David J. Arend
Publikováno v:
53rd AIAA/SAE/ASEE Joint Propulsion Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::aad46f66023122839d9ef883cffddf58
https://doi.org/10.2514/6.2017-5041
https://doi.org/10.2514/6.2017-5041
Autor:
Stefanie M. Hirt
Publikováno v:
53rd AIAA Aerospace Sciences Meeting.
A test was conducted in the 15 cm x 15 cm supersonic wind tunnel at NASA Glenn Research Center that focused on corner effects of an oblique shock-wave/boundary-layer interaction. In an attempt to control the interaction in the corner region, eight co
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c6d2633b0f517ecbf0a0dfde33bdb43f
https://doi.org/10.2514/6.2015-1239
https://doi.org/10.2514/6.2015-1239
Publikováno v:
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
Development of commercial supersonic aircraft has been hindered by many related factors including fuel-efficiency, economics, and sonic-boom signatures that have prevented over-land flight. Materials, propulsion, and flight control technologies have
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::912f08f3abbdd1395ffc294b7723f8ae
https://doi.org/10.2514/6.2014-3802
https://doi.org/10.2514/6.2014-3802
Autor:
Stefanie M. Hirt, Manan A. Vyas
Publikováno v:
51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
Hybrid flow control, a combination of micro-ramps and steady micro-jets, was experimentally investigated in the 15x15 cm Supersonic Wind Tunnel at the NASA Glenn Research Center. A central composite design of experiments method, was used to develop r
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a3e1adfb01f19882fa9b49af6d297601
https://doi.org/10.2514/6.2013-14
https://doi.org/10.2514/6.2013-14
Publikováno v:
50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
Hybrid flow control, a combination of micro-ramps and micro-jets, was experimentally investigated in the 15x15 cm Supersonic Wind Tunnel (SWT) at the NASA Glenn Research Center. Full factorial, a design of experiments (DOE) method, was used to develo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4f25eb6b481d6087a9fa14c380da1254
https://doi.org/10.2514/6.2012-48
https://doi.org/10.2514/6.2012-48