Axisymmetric Transonic Flow Calculations

Axisymmetric Transonic Flow Calculations

L REPT.,SMasson,Bruce S. ;Friedman,Eugene ;DAAA21-72-C-0334PATR-4271(*projectiles, *transonic characteristics), computer programs, wind tunnel models, flow fields, numerical methods and procedures, aerodynamic configurations, shock wavesaxisymmetric bodies, inviscid flowA computer program SONIC 2, w...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Masson,Bruce S, Friedman,Eugene
Format: Report
Sprache:eng
Schlagworte:
AERODYNAMIC CONFIGURATIONS
Ammunition and Explosives
AXISYMMETRIC BODIES
COMPUTER PROGRAMS
FLOW FIELDS
Fluid Mechanics
INVISCID FLOW
NUMERICAL METHODS AND PROCEDURES
PROJECTILES
SHOCK WAVES
TRANSONIC CHARACTERISTICS
WIND TUNNEL MODELS
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Beschreibung
Zusammenfassung:L REPT.,SMasson,Bruce S. ;Friedman,Eugene ;DAAA21-72-C-0334PATR-4271(*projectiles, *transonic characteristics), computer programs, wind tunnel models, flow fields, numerical methods and procedures, aerodynamic configurations, shock wavesaxisymmetric bodies, inviscid flowA computer program SONIC 2, was developed to calculate transonic flow about axisymmetric bodies. The code computes the exact, inviscid compressible flow field with or without shock waves, and it uses a body oriented mesh to permit the exact treatment of an arbitrary body shape. The numerical integration employs the method of Godunov to obtain a stable finite difference approximation to the flow equations. Several examples of results of the code are included along with comparisons to wind tunnel data. (Author)