Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 152
Book Description
Computer Program to Solve Two-dimensional Shock-wave Interference Problems with an Equilibrium Chemically Reacting Air Model
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 152
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 152
Book Description
Computer Program to Solve Two-Dimensional Shock-Wave Interference Problems with an Equilibrium Chemically Reacting Air Model
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722974602
Category :
Languages : en
Pages : 150
Book Description
The computer program EASI, an acronym for Equilibrium Air Shock Interference, was developed to calculate the inviscid flowfield, the maximum surface pressure, and the maximum heat flux produced by six shock wave interference patterns on a 2-D, cylindrical configuration. Thermodynamic properties of the inviscid flowfield are determined using either an 11-specie, 7-reaction equilibrium chemically reacting air model or a calorically perfect air model. The inviscid flowfield is solved using the integral form of the conservation equations. Surface heating calculations at the impingement point for the equilibrium chemically reacting air model use variable transport properties and specific heat. However, for the calorically perfect air model, heating rate calculations use a constant Prandtl number. Sample calculations of the six shock wave interference patterns, a listing of the computer program, and flowcharts of the programming logic are included. Glass, Christopher E. Langley Research Center BOUNDARY LAYER FLOW; COMPUTER PROGRAMS; FLOW DISTRIBUTION; JET IMPINGEMENT; SHOCK HEATING; SHOCK WAVE INTERACTION; ABBREVIATIONS; CONSERVATION EQUATIONS; CYLINDRICAL BODIES; HEAT FLUX; INVISCID FLOW; PRESSURE DISTRIBUTION; REACTION KINETICS; THERMODYNAMIC PROPERTIES...
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722974602
Category :
Languages : en
Pages : 150
Book Description
The computer program EASI, an acronym for Equilibrium Air Shock Interference, was developed to calculate the inviscid flowfield, the maximum surface pressure, and the maximum heat flux produced by six shock wave interference patterns on a 2-D, cylindrical configuration. Thermodynamic properties of the inviscid flowfield are determined using either an 11-specie, 7-reaction equilibrium chemically reacting air model or a calorically perfect air model. The inviscid flowfield is solved using the integral form of the conservation equations. Surface heating calculations at the impingement point for the equilibrium chemically reacting air model use variable transport properties and specific heat. However, for the calorically perfect air model, heating rate calculations use a constant Prandtl number. Sample calculations of the six shock wave interference patterns, a listing of the computer program, and flowcharts of the programming logic are included. Glass, Christopher E. Langley Research Center BOUNDARY LAYER FLOW; COMPUTER PROGRAMS; FLOW DISTRIBUTION; JET IMPINGEMENT; SHOCK HEATING; SHOCK WAVE INTERACTION; ABBREVIATIONS; CONSERVATION EQUATIONS; CYLINDRICAL BODIES; HEAT FLUX; INVISCID FLOW; PRESSURE DISTRIBUTION; REACTION KINETICS; THERMODYNAMIC PROPERTIES...
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 994
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 994
Book Description
STAR
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1230
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1230
Book Description
NASA Tech Briefs
Author:
Publisher:
ISBN:
Category : Technology
Languages : en
Pages : 64
Book Description
Publisher:
ISBN:
Category : Technology
Languages : en
Pages : 64
Book Description
Monthly Catalog of United States Government Publications
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 720
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 720
Book Description
An Implementation of a Chemical and Thermal Nonequilibrium Flow Solver on Unstructured Meshes and Application to Blunt Bodies
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 56
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 56
Book Description
Monthly Catalogue, United States Public Documents
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1786
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1786
Book Description
93-3000 - 93-3034
Author:
Publisher:
ISBN:
Category : Fluid dynamics
Languages : en
Pages : 524
Book Description
Publisher:
ISBN:
Category : Fluid dynamics
Languages : en
Pages : 524
Book Description
AIAA 90-1700 - AIAA 90-1753
Author:
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 436
Book Description
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 436
Book Description