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- Category: AIRCRAF DESIGN (continued)
- Aircraft Direct Operating Cost
- Cost Formulas and Results
- Cost of Parts Fabrication
- Nose Cowl Parts and Subassemblies
- Nacelle Cost Drivers
- Aircraft Costing Methodology: Rapid-Cost Model
- Aircraft Cost and Operational Cost
- What Is to Be Learned?
- Aircraft Cost Considerations
- Military Aircraft Survivability
- End-of-Life Disposal
- Utility Subsystem
- Hydraulic Subsystem
- Electrical Subsystem
- Military Aircraft Application
- Emergency Power Supply
- Aircraft Control Subsystem
- Hands-On Throttle and Stick
- Head-Up Display
- Combat Aircraft Flight Deck
- Multifunctional Display and Electronic Flight Information System
- Aircraft Flight Deck (Cockpit) Layout
- Doors: Emergency Egress
- Aircraft Structural Considerations
- Coursework Overview
- Material Selection
- Material Properties
- Aircraft Materials
- Engine Exhaust Emissions
- Noise Emissions
- Human Interface
- Environmental Issues
- Miscellaneous Design Considerations
- Euler Method Technique
- Large Eddy Simulation (LES) Technique
- Hierarchy of CFD Simulation Methods
- Case Studies
- In the Postprocessor (Menu-Driven)
- Approach to CFD Analyses
- Current Status
- Overview
- The AJT
- The Bizjet
- Maximum Speed Requirements (AJT)
- Climb Performance Requirements (AJT)
- Landing Field Length (AJT)
- Takeoff Field Length (AJT)
- Aircraft Performance Substantiation: Military Aircraft (AJT)
- Payload Range Capability
- Descent Performance (Bizjet)
- Initial High-Speed Cruise (Bizjet)
- Integrated Climb Performance (Bizjet)
- Climb Performance Requirements (Bizjet)
- Landing Field Length (Bizjet)
- Discussion of the Takeoff Analysis
- Takeoff Field Length (Bizjet)
- Aircraft Performance Substantiation: Worked-Out Examples (Bizjet)
- Initial Maximum Cruise Speed
- Climb and Descent Performance
- Balanced Field Length: Civil Aircraft
- Derivation of Pertinent Aircraft Performance Equations
- Maximum Climb Rating (Turboprop): Standard Day
- Takeoff Rating (Turboprop): Standard Day
- Turboprop Engine Performance
- Turbofan Engine (BPR > 4)
- Takeoff Rating (Bizjet): Standard Day
- Establish Engine Performance Data
- Aircraft Speed
- Aircraft Performance
- Active Control Technology: Fly-by-Wire
- Design Considerations for Stability: Civil Aircraft
- Spinning
- Short-Period Oscillation and Phugoid Motion
- Inherent Aircraft Motions as Characteristics of Design
- Current Statistical Trends for H - and V-Tail Coefficients
- Roll Plane
- Yaw Plane
- Pitch Plane
- Lateral Stability: Roll Plane (Roll Moment, L)
- Directional Stability: Yaw Plane (Yaw Moment, N)
- Longitudinal Stability: Pitch Plane (Pitch Moment, M)
- Static and Dynamic Stability
- Stability Considerations Affecting Aircraft Configuration
- Future Growth Potential
- Sizing Analysis: Military Aircraft
- Example: Civil Aircraft
- Variants in the Family of Aircraft Design
- Landing
- 11.4.2 Initial Climb
- Coursework Exercises: Civil Aircraft Design (Bizjet)
- Sizing for Landing Distance
- Sizing to Meet Initial Cruise
- Sizing for the Initial Rate of Climb
- Military Aircraft Design: Takeoff
- Civil Aircraft Design: Takeoff
- Sizing for Takeoff Field Length
- Theory
- 1l| Aircraft Sizing, Engine Matching, and Variant Derivative
- Turbofans with a BPR Around 4 (Smaller Engines; e. g., Bizjets)
- Turbofan Engine: Civil Aircraft