Author: Khaled Sayed Abdol-Hamid
Publisher:
ISBN:
Category :
Languages : en
Pages : 60
Book Description
Development of Three-dimensional Code for the Analysis of Jet Mixing Problem. Part 1: Laminar Solution
Author: Khaled Sayed Abdol-Hamid
Publisher:
ISBN:
Category :
Languages : en
Pages : 60
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 60
Book Description
Development of Three-Dimensional Code for the Analysis of Jet Mixing Problem. Part 1
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722168711
Category :
Languages : en
Pages : 50
Book Description
Future aircraft will eventually feature nonaxisymmetric or rectangular nozzles. Developing a three-dimensional code to stimulate the characteristics of the jet exhaust plume, issuing from nonaxisymmetric nozzles, in general, at different flight conditions, is very important. Two three-dimensional codes were developed to simulate the shock-cell structure of circular nozzles. These codes were developed to solve the parabolized and simplified Navier-Stokes equations respectively. Both codes are based on a method previously developed by Newsome et al. These codes are fully vectorized on the VPS 32 at NASA Langley Research Center. The axisymmetric underexpanded supersonic jet flow problem, exhausting into still air, was used as a test case for developing an efficient three-dimensional problems and preserving crossplane symmetry of the flow downstream of the jet exit. Abdol-Hamid, Khaled S. Unspecified Center NAS1-18599; RTOP 505-62-71-01...
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722168711
Category :
Languages : en
Pages : 50
Book Description
Future aircraft will eventually feature nonaxisymmetric or rectangular nozzles. Developing a three-dimensional code to stimulate the characteristics of the jet exhaust plume, issuing from nonaxisymmetric nozzles, in general, at different flight conditions, is very important. Two three-dimensional codes were developed to simulate the shock-cell structure of circular nozzles. These codes were developed to solve the parabolized and simplified Navier-Stokes equations respectively. Both codes are based on a method previously developed by Newsome et al. These codes are fully vectorized on the VPS 32 at NASA Langley Research Center. The axisymmetric underexpanded supersonic jet flow problem, exhausting into still air, was used as a test case for developing an efficient three-dimensional problems and preserving crossplane symmetry of the flow downstream of the jet exit. Abdol-Hamid, Khaled S. Unspecified Center NAS1-18599; RTOP 505-62-71-01...
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 704
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 704
Book Description
Government Reports Annual Index
Author:
Publisher:
ISBN:
Category : Government reports announcements & index
Languages : en
Pages : 1832
Book Description
Publisher:
ISBN:
Category : Government reports announcements & index
Languages : en
Pages : 1832
Book Description
Papers Presented at the AIAA/ASME/SAE/ASEE 25th Joint Propulsion Conference
Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 472
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 472
Book Description
Computational Prediction of Isolated Performance of an Axisymmetric Nozzle at Mach Number 0.90
Author: John R. Carlson
Publisher:
ISBN:
Category : Fluid dynamics
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Fluid dynamics
Languages : en
Pages : 32
Book Description
NASA SP.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 444
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 444
Book Description
A Multiblock/multizone Code (PAB 3D-v2) for the Three-dimensional Navier-Stokes Equations: Preliminary Applications
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 84
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 84
Book Description
Aeronautical Engineering
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 538
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 538
Book Description
Applied Mechanics Reviews
Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 892
Book Description
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 892
Book Description