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Posts
- Category: When Is A Flow Compressible? (continued)
- Oblique Shock Relations
- Supersonic Flow Over Wedges and Cones
- Shock Interactions and Reflections
- Detached Shock Wave in Front of a Blunt Body
- Prandtl-Meyer Expansion Waves
- Shock-Expansion Theory: Applications to Supersonic Airfoils
- Compressible Flow. Through Nozzles,. Diffusers, and Wind Tunnels
- Governing Equations for Quasi-OneDimensional Flow
- Nozzle Flows
- Diffusers
- Supersonic Wind Tunnels
- Subsonic Compressible Flow over. Airfoils: Linear Theory
- The Velocity Potential Equation
- The Linearized Velocity Potential Equation
- Prandtl-Glauert Compressibility orrection
- Improved Compressibility Corrections
- Critical Mach Number
- A Comment on the Location of Minimum Pressure (Maximum Velocity)
- Drag-Divergence Mach Number: The Sound Barrier
- The Supercritical Airfoil
- CFD Applications: Transonic Airfoils and Wings
- Historical Note: High-Speed Airfoils—Early Research and Development
- Whitcomb—Architect of the Area Rule and the Supercritical Wing
- Linearized Supersonic Flow
- Derivation of the Linearized Supersonic Pressure Coefficient Formula
- Application to Supersonic Airfoils
- Introduction to Numerical. Techniques for Nonlinear. Supersonic Flow
- Elements of the Method of Characteristics
- Internal Points
- 13.2.2 Wall Points
- Supersonic Nozzle Design
- Elements of Finite-Difference Methods
- Predictor Step
- The Time-Dependent Technique: Application to Supersonic Blunt Bodies
- Corrector Step
- Elements of Hypersonic Flow
- Qualitative Aspects of Hypersonic Flow
- Newtonian Theory
- The Lift and Drag of Wings at Hypersonic Speeds: Newtonian Results for a Flat Plate at Angle of Attack
- Accuracy Considerations
- Hypersonic Shock-Wave Relations and Another Look at Newtonian Theory
- Mach Number Independence
- Hypersonics and Computational Fluid Dynamics
- Introduction то the Fundamental Principles and Equations of Viscous Flow
- Qualitative Aspects of Viscous Flow
- Viscosity and Thermal Conduction
- The Navier-Stokes Equations
- The Viscous Flow Energy Equation
- Similarity Parameters
- Solutions of Viscous Flows: A. Preliminary Discussion
- Some Special Cases; Couette and. Poiseuille Flows
- Couette Flow: General Discussion
- Incompressible (Constant Property) Couette Flow
- Negligible Viscous Dissipation
- Equal Wall Temperatures
- Adiabatic Wall Conditions (Adiabatic Wall Temperature)
- Recovery Factor
- Reynolds Analogy
- Interim Summary
- Shooting Method
- Time-Dependent Finite-Difference Method
- Results for Compressible Couette Flow
- Some Analytical Considerations
- Two-Dimensional Poiseuille Flow
- Couette Flow
- Introduction to Boundary Layers
- Boundary-Layer Properties
- The Boundary-Layer Equations
- How Do We Solve the Boundary-Layer Equations?
- Laminar Boundary Layers
- Incompressible Flow over a Flat Plate: The Blasius Solution
- Compressible Flow over a Flat Plate
- A Comment on Drag Variation with Velocity
- The Reference Temperature Method
- Stagnation Point Aerodynamic Heating
- Boundary Layers over Arbitrary Bodies: Finite-Difference Solution
- Finite-Difference Method
- Turbulent Boundary Layers
- Results for Turbulent Boundary Layers on a Flat Plate
- Reference Temperature Method for Turbulent Flow
- Turbulence Modeling
- Final Comments
- Examples
- Examples of Some Solutions
- Flow over an Airfoil
- Flow over a Complete Airplane
- Shock-Wave/Boundary-Layer Interaction
- Flow over an Airfoil with a Protuberance
- The Issue of Accuracy for the Prediction of Skin Friction Drag