Zobrazeno 1 - 10
of 13
pro vyhledávání: '"Jim C Narramore"'
Autor:
Chunhua Sheng, Jim C Narramore
Publikováno v:
Journal of Aircraft. 45:971-980
The unsteady flowfield of a Bell-Agusta 609 rotor is numerically investigated with an unsteady Reynolds-averaged Navier-Stokes flow solver based on unstructured grid topology. The geometry considered is a three-bladed rotor that is undergoing a highe
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::574dee8fa145310d8cee53485f957725
https://doi.org/10.2514/1.32877
https://doi.org/10.2514/1.32877
Publikováno v:
Journal of Aircraft. 44:1805-1814
Two new mechanisms for downstream ice growth (i.e., downstream of the primary ice shape) in aircraft icing scenarios were investigated. The first mechanism is local variation of relative humidity with its potential for water deposition due to supersa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2862531b829f3a53cd866598f5d2eaab
https://doi.org/10.2514/1.28794
https://doi.org/10.2514/1.28794
Autor:
Chunhua Sheng, Nischint Rajmohan, Lakshmi N. Sankar, Jim C. Narramore, Qiuying Zhao, John O. Bridgeman
Publikováno v:
49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
An unstructured hybrid approach is developed aimed at computing viscous flows around helicopter rotors in hover and forward flight. A single rotor blade is resolved through the Navier-Stokes solution with the consideration of the blade vortex interac
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ad29148411500497ec2d0c1950434982
https://doi.org/10.2514/6.2011-1124
https://doi.org/10.2514/6.2011-1124
Autor:
Jim C Narramore, R. Vermeland
Publikováno v:
Journal of Aircraft. 29:73-78
Momentum blade element methods, which have historically been used to predict rotor blade thrust, underpredict the power that is required for highly twisted rotors at high thrust levels. During a test of the V-22 tilt rotor blade conducted at the NASA
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::62746d6f649e815608c3abb5cdb9edc9
https://doi.org/10.2514/3.46127
https://doi.org/10.2514/3.46127
Publikováno v:
Journal of Aircraft. 28:216-224
An airfoil design procedure is described that was incorporated into an existing 2-D Navier-Stokes airfoil analysis method. The resulting design method, an iterative procedure based on a residual-correction algorithm, permits the automated design of a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::abde6861976f4c31fd11a4c3b5a9622d
https://doi.org/10.2514/3.46015
https://doi.org/10.2514/3.46015
Publikováno v:
12th AIAA/CEAS Aeroacoustics Conference (27th AIAA Aeroacoustics Conference).
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c65d536bf8fef60a2f7d3ee8a14ef78d
https://doi.org/10.2514/6.2006-2603
https://doi.org/10.2514/6.2006-2603
Publikováno v:
SAE Technical Paper Series.
Even though aircraft icing has been an active area of research for many years due to its public safety ramifications, there are still gaps in the knowledge base, such as in the ice accretion process. Ice prediction codes have been developed and gener
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cd108f9dd61817b05c3c901896954500
https://doi.org/10.4271/2005-01-3375
https://doi.org/10.4271/2005-01-3375
Publikováno v:
42nd AIAA Aerospace Sciences Meeting and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9e54e05411c17df62d55f1fa73b092f3
https://doi.org/10.2514/6.2004-59
https://doi.org/10.2514/6.2004-59
Publikováno v:
SAE Technical Paper Series.
The FENSAP-ICE system was first conceived for fixed-wing aircraft and air induction system icing, but major developments are underway to augment its capabilities for icing simulation of rotorcraft and tiltrotor aircraft. A project is underway, under
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::157ea8d5b47e997ae0505a12f2514e30
https://doi.org/10.4271/2003-01-2105
https://doi.org/10.4271/2003-01-2105
Publikováno v:
41st Aerospace Sciences Meeting and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1eb0e2bae95f851d3262289ae8031eec
https://doi.org/10.2514/6.2003-24
https://doi.org/10.2514/6.2003-24