Zobrazeno 1 - 10
of 36
pro vyhledávání: '"Adam Rasheed"'
Autor:
Haroon Adam Rasheed, BS, Tyler Davis, MS, Esteban Morales, MS, Zhe Fei, MS, PhD, Lourdes Grassi, MD, Agustina De Gainza, MD, Kouros Nouri-Mahdavi, MD, MS, Joseph Caprioli, MD
Publikováno v:
Ophthalmology Science, Vol 3, Iss 2, Pp 100255- (2023)
Purpose: To report an image analysis pipeline, DDLSNet, consisting of a rim segmentation (RimNet) branch and a disc size classification (DiscNet) branch to automate estimation of the disc damage likelihood scale (DDLS). Design: Retrospective observat
Externí odkaz:
https://doaj.org/article/a378cd1c45074c6eaf6aecbbb65ec90d
Autor:
Haroon Adam Rasheed, BS, Tyler Davis, MS, Esteban Morales, MS, Zhe Fei, MS, PhD, Lourdes Grassi, MD, Agustina De Gainza, MD, Kouros Nouri-Mahdavi, MD, MS, Joseph Caprioli, MD
Publikováno v:
Ophthalmology Science, Vol 3, Iss 1, Pp 100244- (2023)
Purpose: Accurate neural rim measurement based on optic disc imaging is important to glaucoma severity grading and often performed by trained glaucoma specialists. We aim to improve upon existing automated tools by building a fully automated system (
Externí odkaz:
https://doaj.org/article/88f1bfb9aec4428b9f3fd1dae9c1cdcc
To report the availability and activity of online uveitis support groups. An online search was conducted for support groups for uveitis. Member count and activity were recorded. Posts and comments were graded along five themes: emotional or personal
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::83451b35cb354f154245bd3c5f35fdd8
Autor:
Haroon Adam Rasheed, Tyler Davis, Esteban Morales, Zhe Fei, Lourdes Grassi, Agustina De Gainza, Kouros Nouri-Mahdavi, Joseph Caprioli
Publikováno v:
Ophthalmology science, vol 3, iss 1
PurposeAccurate neural rim measurement based on optic disc imaging is important to glaucoma severity grading and often performed by trained glaucoma specialists. We aim to improve upon existing automated tools by building a fully automated system (Ri
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::ce22256fd3765ce6d643b3b8c8a8d881
https://pubmed.ncbi.nlm.nih.gov/36545262
https://pubmed.ncbi.nlm.nih.gov/36545262
Publikováno v:
The Journal of ECT. 38:262-263
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::e39f945cb990756bb62c3e1607042643
https://doi.org/10.1097/yct.0000000000000871
https://doi.org/10.1097/yct.0000000000000871
Publikováno v:
Journal of Propulsion and Power. 27:586-596
A multitube pulse detonation combustor consisting of eight unvalved tubes arranged in a can-annular configuration was integrated with a single-stage axial turbine nominally rated for 10 lbm=s, 25,000 rpm and 1000 hp. The multitube pulse-detonation-co
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f039389ed411513ce97a8d1e5021d034
https://doi.org/10.2514/1.b34013
https://doi.org/10.2514/1.b34013
Publikováno v:
Scopus-Elsevier
A parametric study into the integration of a pulse detonation engine (PDE) with an ejector was performed. High-speed shadowgraph visualizations of the flow inside the two-dimensional ejector provided a qualitative method of determining the performanc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::01d4c36303524eb4279f308836fd5b92
https://doi.org/10.2514/1.8125
https://doi.org/10.2514/1.8125
Publikováno v:
AIAA Journal. 39:605-610
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::47b6675f1c9c236e578ff93889d864e1
https://doi.org/10.2514/3.14776
https://doi.org/10.2514/3.14776
Publikováno v:
47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition.
*† ‡ § Experimental measurements of static pressure -rise and thrust are made in a pulse deton ation engine (PDE). The research employs a valved ethylene -air 3 -tube PDE at an operating frequency of 20 Hz per tube. New terminology and definitio
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cf635646c366479c8f9954d0d9f3dc89
https://doi.org/10.2514/6.2009-857
https://doi.org/10.2514/6.2009-857
Autor:
Adam Rasheed, Venkat Eswarlu Tangirala, Robert A. Dunton, Justin Thomas Brumberg, Aaron Jerome Glaser
Publikováno v:
44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
A thrust stand capable of measuring the time averaged thrust produced by a PDE was designed and tested. The study quantified the effect of exit nozzles on a valved multi-tube PDE system with three tubes arranged in a close-packed configuration. Three
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8dcd0d291630d55782c01b921f32db65
https://doi.org/10.2514/6.2008-4692
https://doi.org/10.2514/6.2008-4692