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Posts
- Category: AIRCRAF DESIGN (continued)
- Load on Wheels
- Loads on Wheels and Shock Absorbers
- Turning of an Aircraft
- Undercarriage Design Drivers and Considerations
- Stowage Space Clearances
- Undercarriage Retraction and Stowage
- Undercarriage Layout, Nomenclature, and Definitions
- Types of Undercarriage
- Undercarriage
- Configuring Military Aircraft - Shaping and Laying Out
- Miscellaneous Considerations in Civil Aircraft
- Worked-Out Example: Finalizing the Preliminary Civil Aircraft Configuration
- Undercarriage Positioning
- Worked-Out Example: Configuring and Positioning the Engine and Nacelle in Civil Aircraft
- Configuring a Civil Aircraft Nacelle: Positioning and Layout of an Engine
- Worked-Out Example: Configuring the Empennage in Civil Aircraft
- Horizontal Tail
- Configuring a Civil Aircraft Empennage: Positioning and Layout
- Worked-Out Example: Configuring the Wing in Civil Aircraft
- Positioning of the Wing Relative to the Fuselage
- Wing-Mounted Control-Surface Layout
- Wing Sweep
- Planform Shape
- 6.5.2 Wing Design
- Configuring a Civil Aircraft Wing: Positioning and Layout
- Worked-Out Example: Civil Aircraft Fuselage Layout
- Wide-Body, Double-Aisle Aircraft
- Narrow-Body, Single-Aisle Aircraft
- Civil Aircraft Fuselage: Typical Shaping and Layout
- Considerations in Configuring the Nacelle
- Considerations in Configuring the Empennage
- Considerations in Configuring the Wing
- Closure of the Fuselage
- Considerations in Configuring the Fuselage
- Introduction
- What Is to Be Learned?
- Configuring Aircraft
- Gust Envelope
- Negative Loads
- Extreme Points of a V-n Diagram
- Low-Speed Limit
- Maximum Limit of Load Factor
- Limits - Load and Speeds
- Theory and Definitions
- On the Ground
- Roll Plane (Y-Z) Maneuver (Aileron-Induced)
- Flight Maneuvers
- Buffet
- Aircraft Load
- Military Aircraft: Detailed Classification, Evolutionary Pattern, and Mission Profile
- Summary of Civil Aircraft Design Choices
- Nacelle Group
- Empennage Group (Civil Aircraft)
- Wing Group
- Doors - Emergency Exits
- Cargo Container Sizes
- Passenger Facilities
- Seat Arrangement, Pitch, and Posture (95th Percentile) Facilities
- Flight Crew (Flight Deck) Compartment Layout
- Front (Nose Cone) and Aft-End Closure
- Fuselage Length
- Fuselage Group
- Civil Aircraft Component Geometries
- Empennage Area versus Wing Area
- Maximum Takeoff Mass versus Engine Power
- Maximum Takeoff Mass versus Wing Area
- Maximum Takeoff Mass versus Fuel Load
- Maximum Takeoff Mass versus Operational Empty Mass
- Maximum Takeoff Mass versus Number of Passengers
- Civil Subsonic Jet Aircraft Statistics (Sizing Parameters and Regression Analysis)
- Civil Aircraft Mission (Payload-Range)
- Aircraft Classification and Their Operational Environment
- Aircraft Evolution
- Aircraft Classification, Statistics, and Choices for Configuration
- Speed Brakes and Dive Brakes
- Undercarriage
- Average Diameter, Dave
- Aft Fuselage Closure Length, La
- Fuselage Closure Angle
- Fuselage Length, Lfus
- Fuselage
- Canard Configuration
- V-Tail Volume Coefficient, Cvt
- Tail Volume Coefficients
- H-Tail
- Empennage
- Finalizing Wing Design Parameters
- Additional Surfaces on Wing
- Additional Vortex Lift
- The Square-Cube Law
- Influence of Wing Area and Span on Aerodynamics
- Wing Stall Pattern and Wing Twist
- Compressibility Effect: Wing Sweep
- Dihedral/Anhedral Angles
- Wing Taper Ratio, X
- Wing Aspect Ratio
- Wing Definitions
- Aspect Ratio Correction of 2D Aerofoil Characteristics for 3D Finite Wing
- Induced Drag and Total Aircraft Drag
- Wing Aerodynamics