Cena: |
Želi ovaj predmet: | 3 |
Stanje: | Polovan bez oštećenja |
Garancija: | Ne |
Isporuka: | Pošta Post Express Lično preuzimanje |
Plaćanje: | Tekući račun (pre slanja)
Lično |
Grad: |
Šabac, Šabac |
ISBN: Ostalo
Godina izdanja: 1996
Autor: Domaći
Jezik: Engleski
Oblast: Mašinstvo
58963) TRANSONIC AERODYNAMICS NUMERICAL ANALYSIS , Petrović Z. , Stupar S. , Mechanical Engineering Faculty University of Belgrade 1996 ;
Contents :
1 Introduction
1.1 Preliminary Remarks.
1.2 Governing Equations
1.3 Simplifications to the Governing Equations
1.3.1 Definition of an Adiabatic Flow.
1.3.2 Definition of an Irrotational Flow
1.3.3 Crocco`s Theorem
1.3.4 Isentropic Gas Relation
1.4 Algebraic Form of Energy Equation for Steady Adiabatic Flow
1.5 The Isentropic Form of the Energy Equation
1.6 The Momentum Conservation Laws.
1.7 Isentropic Shocks vs. `Real World Shocks`
1.7.1 Rankine-Hugoniot approach
1.7.2 Isentropic approach
1.8 Techniques for Handling Shocks in Potential Flow Calculations
1.9 Summary
2 Transonic Small Disturbance Equation
2.1 Preliminary Remarks.
2.1.1 Treatment of Flow Angle of Attack
2.2 Definition of Disturbance Potential
2.3 Boundаry Conditions for Flow at the Body Surface
2.4 Derivation of the TSD Equation
2.5 Properties of the TSD Equation.
2.6 Finite Difference Terminology
2.7 Conservation Form vs. Non-Conservation Form
2.8 Finite Difference Expression Form of the TSD Equation in Subsoni
2.9 Murman-Cole Switching in supersonic Regions
2.10 Discretization Error Associated with Equation (2.2)
2.11 Loss of Conservation Property due to Switching
2.12 Murman-Cole Switching in Conservation Form
2.13 Application of Boundary Conditions
2.13.1 Region Ahead of the Leading Edge: (1