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- Category: Modeling and Simulation of Aerospace Vehicle Dynamics (continued)
- Straight Line
- Displacement of Points
- Modeling of Geometry
- Dyadic Product
- Vector Product
- Scalar Product
- Tensor Algebra
- Cartesian Tensors
- Coordinate Systems
- Tensor Elements
- Notation
- Building Blocks of Mathematical Modeling
- Principle of Material Indifference
- Axioms of Classical Mechanics
- Elements of Classical Mechanics
- Mathematical Concepts in Modeling
- Simulation of Aerospace Vehicles
- Modeling of Flight Dynamics
- Virtual Engineering
- Modeling and Simulation of Aerospace Vehicle Dynamics
- Category: NEW DESIGN CONCEPTS FOR HIGH SPEED AIR TRANSPORT
- Results
- Nonlinear Theory
- McDonnell Douglas Studies
- NASA Studies
- Boeing Studies
- Stanford Studies
- Other Oblique Flying Wing Studies
- The OFW as the NLA
- Linear Theory
- OBLIQUE FLYING WING STUDIES
- Economy
- Ozone
- Sonic Boom
- . Environmental Impact
- Proof of Concept Demonstrators
- Stability and Control
- Structural Loads and Weights
- Aerodynamics
- Baseline Design and Layout
- Overview
- THE OBLIQUE FLYING WING TRANSPORT
- Supersonic Laminar Flow Flight Tests
- Wind Tunnels for Supersonic Laminar Flow
- Theoretical Prediction of Supersonic Transition
- Supersonic Transition Physics
- Laminarisation of Supersonic Transports
- Future Supersonic Commercial Transports
- LAMINAR FLOW FOR SUPERSONIC TRANSPORTS
- . Technology Assessment
- Variation of Range, Mach number and Payload
- Reference Aircraft
- Variables and Constraints
- Global Model Technology Base
- Application of the Method to Supersonic Civil Transports
- Present Method Issues
- MIDAS: A Design Process
- Overview
- MULTI-DISCIPLINARY SUPERSONIC TRANSPORT DESIGN
- Using Optimization
- Optimized European Supersonic Transport
- Examples
- Analysis
- Constraints
- Variables
- General Methodology
- SUPERSONIC AIRCRAFT SHAPE OPTIMIZATION
- Suggested General Structure of the MIDO Algorithms
- Parallelization and Networking Issues
- Convergence Acceleration and Reliability Enhancement
- Computational Grid Generation
- MULTIDISCIPLINARY INVERSE DESIGN AND OPTIMIZATION (MIDO)
- Inverse Determination of Elastostatic Boundary Conditions
- Inverse Problems in Elastostatics
- STRUCTURAL INVERSE DESIGN AND OPTIMIZATION
- Determination of Convective Heat Transfer Coefficients on Surfaces of Coolant Passages
- Optimization of Thicknesses of Walls and Interior Struts
- Minimization of the Number of Coolant Flow Passages
- Optimization of Surface Heat Fluxes and Temperatures for Minimum Coolant Flow Rate
- General Design Objectives
- Determination of Steady Thermal Boundary Conditions
- Determination of Number, Sizes, Locations, and Shapes of Coolant Flow Passages
- THERMAL INVERSE DESIGN AND OPTIMIZATION
- Control Theory (Adjoint Operator) Approach
- COMBINED OPTIMIZATION AND INVERSE DESIGN. OF 3-D AERODYNAMIC SHAPES
- Hybrid GA/Gradient Search Constrained Optimization
- Constrained Genetic Evolution Optimization
- Optimization Using Sensitivity Derivatives
- AERODYNAMIC SHAPE OPTIMIZATION METHODS
- Integro-Differential Equation Concept
- Characteristic Boundary Condition Concept
- Direct Surface Transpiration Concept
- Indirect Surface Transpiration Concept
- Elastic Surface Motion Concept
- Stream-Function-Coordinate (SFC) Concept
- Surface Flow Data Specification
- AERODYNAMIC SHAPE INVERSE DESIGN METHODS
- Novel Configurations
- Software development for CFD and CAD preprocessing
- Coupling with visualization tools