Our heavyweight helicopter equal in the world does not have
In Rostov started production of the most load-lifting rotary-wing car The Russian holding «Helicopt[...]
Special Recent Posts
In Italy broke experimental tiltrotor
The experimental military man конвертоплан, developed by "August Vestland's" company, brok[...]
The old plane — nonsense, pilots think - there was an attack
In spite of the fact that the main version of crash of the Russian plane of the Kogalymavia company [...]
The Israeli Apache will subject to peeling
The Israeli shock Boeing AH-64 Apache helicopters will undergo "peeling" procedure. As rep[...]
The aviation industry began to move
On Monday against Dubai Airshow air show - the 2015th Deputy Prime Minister Dmitry Rogozin blew up t[...]
Sitemap
Posts
- Category: AIRCRAF DESIGN (continued)
- Transonic Effects - Area Rule
- High-Lift Devices
- Comparison of Three NACA Aerofoils
- Gradual Stall
- Types of Stall
- Generation of Lift
- Definitions of Aerodynamic Parameters
- Other Types of Aerofoils
- NACA Five-Digit Aerofoil
- Groupings of Aerofoils and Their Properties
- Aerofoil
- Forces
- Aircraft Motion and Forces
- Flow Past Aerofoil
- Airflow Behavior: Laminar and Turbulent
- Fundamental Equations
- Introduction
- Aerodynamic Considerations
- Coursework Procedures
- Airworthiness Requirements
- Comparison between Civil and Military Aircraft Design Requirements
- Military Market
- Aircraft Specifications and Requirements for Three Civil Aircraft Case Studies
- Civil Aircraft Market
- Military Aircraft and Its Component Configurations
- Civil Aircraft and Its Component Configurations
- Aircraft Familiarization
- Project Activities for Small Aircraft Design
- Functional Tasks during the Conceptual Study (Phase 1: Civil Aircraft)
- Phase 1: Conceptual Study Phase (Feasibility Study)
- Typical Cost Frame
- Typical Resources Deployment
- . Four Phases of Aircraft Design
- Typical Design Process
- Coursework Content
- What Is to Be Learned?
- Methodology to Aircraft Design, Market Survey, and Airworthiness
- Cost Implications
- Units and Dimensions
- Military Aircraft Design: Future Trends
- Civil Aircraft Design: Future Trends
- Current Military Aircraft Design Trends
- Current Civil Aircraft Design Trends
- Current Aircraft Design Status
- Brief Historical Background
- Introduction
- Use of Semi-empirical Relations
- Suggestions for the Class
- Road Map of the Book
- Aircraft Design
- Category: Aircraft Flight
- Lift
- The conventional wing
- The generation of lift
- Optimum economy with the jet engine
- Centre of gravity movement
- Aircraft Flight
- Moving aircraft and moving air
- The aerofoil section
- Air pressure density and temperature
- Pressure and speed
- Dynamic pressure
- Unexpected effects
- The wing-bound vortex
- The Magnus effect
- The air flow around an aerofoil section
- Stagnation
- Pressure and lift
- The direction of the resultant force due to pressure
- Variation of lift with angle of attack and camber
- Variation of CL with flight conditions
- Stalling
- Flight with separated flow
- Other methods of lift generation
- Lift generation using engine thrust
- Lift from rotating wings
- High speed helicopters and convertiplanes
- The autogyro
- Spoiled for choice
- Wing planform
- The generation of lift by a wing
- Trailing vortex formation
- The starting vortex
- Downwash and its importance
- The influence of aspect ratio
- Variation of lift along the span
- Wing plan shape
- Planform and handling, wing-tip stalling
- Swept wings
- Disadvantages of swept wings
- Delta wings
- Highly swept and slender delta wings
- Other wing planforms
- Biplanes and multiplanes
- The joined wing
- The boundary layer and its control
- The boundary layer
- How the boundary layers form
- Flow separation and stalling
- Favourable and unfavourable conditions