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Posts
- Category: AIRCRAF DESIGN (continued)
- Maximum Climb Rating
- Turboprop Engine (Up to 100 Passengers Class)
- Piston Engine
- Maximum Continuous Rating
- Engine-Performance Data
- Propeller Performance: Blade Numbers 3 < N > 4
- Propeller Performance: Practical Engineering Applications
- Blade-Element Theory
- Propeller Theory
- Propeller-Related Definitions
- Military Aircraft Thrust Reverser Application and Exhaust Nozzles
- Coursework Example of Civil Aircraft Nacelle Design
- Civil Aircraft Exhaust Nozzles
- Civil Aircraft Thrust Reverser Application
- Military Aircraft Intake Design
- Civil Aircraft Intake Design: Inlet Sizing
- Intake and Nozzle Design
- Combat Aircraft Engine Installation
- Turboprop Integration to Aircraft
- Subsonic Civil Aircraft Nacelle and Engine Installation
- Turboprop Engine: Formulation
- Afterburner Engine: Formulation
- Bypass Turbofan Engine: Formulation
- Simple Straight-Through Turbojet Engine: Formulation
- Simplified Representation of the Gas Turbine Cycle
- Piston Engine
- Turboprop Engine
- Afterburner Engine
- Turbofan: Bypass Engine
- Introduction: Air-Breathing Aircraft Engine Types
- Definitions
- Background
- Overview
- Total Aircraft Drag
- ACDp Estimation
- Summary of Parasite Drag
- Computation of 3D and Other Effects to Estimate Component Copmin A component-by-component example follows
- Computation of Wetted Areas, Re, and Basic CF
- Geometric and Performance Data of a Vigilante RA-C5 Aircraft
- Summary of Parasite Drag
- Coursework Example: Civil Bizjet Aircraft
- Supersonic Drag
- Military Aircraft Drag
- One-Engine Inoperative Drag
- Dive Brakes and Spoilers Drag
- High-Lift Device Drag
- Total Aircraft Drag
- Subsonic Wave Drag
- Minimum Parasite Drag
- Miscellaneous Parasite Drags
- Excrescence Drag
- Base Drag
- Intake Drag
- Nacelle Drag
- Wing, Empennage, Pylons, and Winglets
- Semi-empirical Relations to Estimate Aircraft Component Parasite Drag
- Stepwise Approach to Compute Minimum Parasite Drag
- Computation of Wetted Areas
- Geometric Parameters, Reynolds Number, and Basic CF Determination
- Minimum Parasite Drag Estimation Methodology
- Aircraft Drag Estimation Methodology (Subsonic)
- Aircraft Drag Formulation
- Aircraft Drag Breakdown (Subsonic)
- Parasite Drag Definition
- Aircraft Drag
- Graphical Method to Predict Aircraft Component Weight - Military Aircraft
- First Iteration to Fine Tune CG Position Relative to Aircraft and Components
- Bizjet Aircraft CG Location Example
- Center of Gravity Determination
- Systems Group Mass
- Nacelle Group Mass
- Wing Group Mass
- Fuselage Group Mass
- Fuel - Civil Aircraft
- Payload - Civil Aircraft
- Furnishing Group - Civil Aircraft
- Miscellaneous Group - Civil Aircraft
- Undercarriage Group - Civil Aircraft
- Empennage Group - Civil Aircraft
- Wing Group - Civil Aircraft
- Fuselage Group - Civil Aircraft
- Semi-empirical Equation Method (Statistical)
- Graphical Method for Predicting Aircraft Component Weight: Civil Aircraft
- Rapid Mass Estimation Method: Civil Aircraft
- Military Aircraft (Combat Category)
- Aircraft Component Groups
- Desirable CG Position
- Aircraft Mass (Weight) Breakdown
- The Weight Drivers
- Aircraft Weight and Center of Gravity Estimation
- Miscellaneous Considerations
- Military Aircraft: AJT
- Worked-Out Examples
- Undercarriage Layout Methodology
- Tire Friction with Ground: Rolling and Braking Friction Coefficient
- Tires
- Aircraft Classification Number and Pavement Classification Number Method
- Load Classification Number Method
- Runway Pavement Classification
- Energy Absorbed