Zobrazeno 1 - 10
of 15
pro vyhledávání: '"Steven C. Caruso"'
Autor:
Michael R. Mendenhall, Marnix F. E. Dillenius, Steven C. Caruso, Gary D. Kuhn, Daniel J. Lesieutre
Publikováno v:
Journal of Spacecraft and Rockets. 31:1007-1015
Pegasus™, a three-stage, air-launched, winged space booster, was developed to provide fast and efficient commercial launch services for small satellites. The aerodynamic design and analysis of the vehicle were conducted without wind-tunnel and subs
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6ec6893288f1e7b28d8ef36242defb2d
https://doi.org/10.2514/3.26551
https://doi.org/10.2514/3.26551
Autor:
Steven C. Caruso, Robert E. Childs
Publikováno v:
Journal of Propulsion and Power. 7:607-616
The accuracy of Reynolds-aver aged Navier-Stokes calculations of axisymmetric high-speed afterbody flows is investigated. An approximate truncation error analysis is used to identify specific regions where discretization errors are large, and grid re
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4d3eb9e9a5ea130ac13aa3b6437cd664
https://doi.org/10.2514/3.23369
https://doi.org/10.2514/3.23369
Publikováno v:
Acta Mechanica. 86:15-29
It is known that the nonlinear Navier-Stokes equations will model most fluid flow of aeronautical interest. The existence and uniqueness of the solutions to the Navier-Stokes equations have not been proven although it is known that in certain cases o
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::661ce4dceeaaf3969f63fecb3e45e60d
https://doi.org/10.1007/bf01175946
https://doi.org/10.1007/bf01175946
Autor:
Steven C. Caruso
Publikováno v:
32nd Aerospace Sciences Meeting and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::28826c012437b7020c40b0edf39b666b
https://doi.org/10.2514/6.1994-486
https://doi.org/10.2514/6.1994-486
Autor:
Steven C. Caruso
Publikováno v:
32nd Aerospace Sciences Meeting and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c7b29be56fc9655c5ba13a173da285e0
https://doi.org/10.2514/6.1994-606
https://doi.org/10.2514/6.1994-606
Autor:
Steven C. Caruso
Publikováno v:
31st Aerospace Sciences Meeting.
A parallel computer implementation (128 processors) of LEWICE, a NASA Lewis code used to predict the time-dependent ice accretion process for two-dimensional aerodynamic bodies of simple geometries, is described. Two-dimensional parallel droplet traj
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a5a643654907a8a7f818e6049cd2aa90
https://doi.org/10.2514/6.1993-172
https://doi.org/10.2514/6.1993-172
Autor:
Mohammad Farshchi, Steven C. Caruso
Publikováno v:
30th Aerospace Sciences Meeting and Exhibit.
This paper describes a flowfield mesh generation procedure which has been developed specifically for dealing with geometrically complex and time-dependent leading edge ice accretions on airfoils. The method produces an unstructured mesh using an auto
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a4c6ae0a924343b04b5c03d4802d6e2c
https://doi.org/10.2514/6.1992-415
https://doi.org/10.2514/6.1992-415
Publikováno v:
30th Aerospace Sciences Meeting and Exhibit.
This final report documents the results of a study demonstrating the use of analytical computational fluid dynamics methods to predict the aerodynamic characteristics and flowfield details of a typical ejection seat with an occupant. This feasibility
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2a387e80743c188d04dd543d12d23c31
https://doi.org/10.2514/6.1992-403
https://doi.org/10.2514/6.1992-403
Autor:
Marnix F. E. Dillenius, Steven C. Caruso, Gary D. Kuhn, Daniel J. Lesieutre, Michael R. Mendenhall
Publikováno v:
29th Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3f53c9647f4ddd1c241ac58c855bd92f
https://doi.org/10.2514/6.1991-190
https://doi.org/10.2514/6.1991-190
Autor:
Steven C. Caruso
Publikováno v:
28th Aerospace Sciences Meeting.
An advanced flowfield prediction method for airfoils with leading edge ice accretions was developed and applied. The method is intended to be eventually used in an aircraft icing analysis. The flowfield is obtained by solving the Euler or Navier-Stok
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c7ac9ec55d4dcf2d2825b3ca830edb70
https://doi.org/10.2514/6.1990-758
https://doi.org/10.2514/6.1990-758