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Posts
- Category: Basics of Aero - thermodynamics (continued)
- Laminar-Turbulent Transition and Turbulence in High-Speed Viscous Flow
- Case Study: Wall Temperature and Skin Friction at the SANGER Forebody
- The Thermal State of Flat Surface Portions
- Wall Shear Stress at Flat Surface Portions
- Boundary-Layer Thickness at Stagnation Points and Attachment Lines
- Boundary-Layer Thicknesses and Integral Parameters
- Basic Properties of Attached Viscous Flow
- Equations of Motion for Hypersonic Attached Viscous Flow
- The Reference Temperature/Enthalpy Method for Compressible Boundary Layers
- Wall Compatibility Conditions
- Global Characteristic Properties of Attached Viscous Flow
- Boundary-Layer Equations
- Some Properties of Three-Dimensional Attached Viscous Flow
- Attached Viscous Flow
- Attached High-Speed Viscous Flow
- The Mach-Number Independence Principle of Oswatitsch
- Modification Schemes, Application Aspects
- Newton Flow
- The Change of the Unit Reynolds Number across Shock Waves
- Supersonic Turning: Prandtl-Meyer Expansion and Isentropic Compression
- The Entropy Layer at a Blunt Body
- Blunt-Body Flow
- Treatment of Shock Waves in Computational Methods
- The Oblique Shock Wave
- Shock Waves
- One-Dimensional Shock-Free Flow
- Hypersonic Flight Vehicles and Shock Waves
- Inviscid Aerothermodynamic Phenomena
- Computation Models
- A Few Remarks on Simulation Issues
- Surface Catalytic Recombination
- Nozzle Flow in a “Hot” Ground-Simulation Facility
- Rate Effects, Two Examples
- Thermal and Chemical Rate Processes
- Dissociation and Recombination
- High-Temperature Real-Gas Effects
- Van der Waals Effects
- Real-Gas Aerothermodynamic Phenomena
- Remarks on Similarity Parameters
- Transport of Mass
- Transport of Energy
- Equations of Motion, Initial Conditions, Boundary Conditions, and Similarity Parameters
- Computation Models
- Mass Diffusivity
- Thermal Conductivity
- Viscosity
- Transport Properties
- Transport Phenomena
- Transport of Momentum, Energy, and Mass
- Summary of the Results of the Chapter in View of Flight-Vehicle Design
- The Computed Radiation-Adiabatic Temperature Field
- Topology of the Computed Skin-Friction and Velocity Fields
- Configuration and Computation Cases
- Case Study: The Thermal State of the Surface of the Blunt Delta Wing
- Some Parametric Considerations of the Radiation-Adiabatic Temperature
- Scaling of the Radiation-Adiabatic Temperature
- Non-convex Effects
- Qualitative Behavior of the Radiation-Adiabatic Temperature on Real Configurations
- Local Analysis of Radiation Cooling
- The Radiation-Adiabatic Vehicle Surface
- Definitions
- Thermal Radiation Cooling of External Vehicle Surfaces
- Problems
- Flow Regimes
- The Flight Environment
- Scope and Content of the Book
- Unsteady Flight and Steady Aerothermodynamics?
- The Thermal State of the Surface and Thermal Surface Effects
- The Tasks of Aerothermodynamics
- RV-Type and CAV-Type Flight Vehicles as Reference Vehicles
- Basics of Aerothermodynamics
- Category: Canonical impulse solutions
- Natural response
- Linearized equations of motion
- Flight Dynamics Formulation
- Dynamics Relations
- Aircraft Kinematic Relations
- Flow Angles
- Axis Parameterization and Conventions
- Axis Systems
- Introduction to Flight Dynamics
- Optimum unswept wing
- Transonic airfoils Airfoil performance characterization
- TSD equation analysis
- Transonic Flows
- Supersonic lifting flows Supersonic lift singularities
- Wave drag of arbitrary slender bodies of revolution
- . Canonical supersonic flow
- Small-Disturbance Supersonic Flows
- Compressible 3D far-field
- Compressible 2D far-field
- Subsonic Compressible Far-Fields
- Compressible infinite swept wing
- Low-speed infinite swept wing
- Compressible 3D finite wing
- Prandtl-Glauert equation solution procedure
- Prandtl-Glauert Analysis
- . Ranges of validity
- Perturbation potential flows
- Second-order approximations