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Posts
- Category: Propellor Aerodynamics (continued)
- Solidity
- Power Absorption
- Power to the Prop
- Propulsive Efficiency
- - Thrust & Efficiency
- Variable Pitch & Constant Speed Propellers
- Fixed-pitch Propellers
- Advance/Diameter Ratio
- Brief Review
- Slip
- Geometric Pitch
- Experimental Pitch
- The Working Fluid
- - Propeller Pitch
- Propfans
- Propulsors
- Supersonic Propellers
- The First Turboprops
- Propeller Manufacturers
- De-ice for Props
- Lockheed C-130 Hercules
- Counter & Contra-rotating Props
- Five-blades or Six?
- Spitfires and Hurricanes
- Constant-speed Propellers
- Variable-pitch Propellers
- Aerodynamic Theories
- The Wright Brothers
- The First Airborne Props
- - The History of Aircraft Propellers
- Category: Ruder am Fliigel endlicher Spannweite 12.31 Ruder am Fliigel bei inkompressibler Stromung
- Category: The Aerodynamic Design of Aircraft
- CONCLUSIONS AND OUTLOOK
- Propulsive lifting bodies
- Heat addition to airstrearns
- Effects of viscosity
- Off-design characteristics
- Design of lifting bodies from known flowfields
- WAVERIDER AIRCRAFT
- Design considerations
- Performance considerations
- SLENDER AIRCRAFT FOR FLIGHT AT SUBSONIC. SPEEDS OVER SHORT RANGES
- Lifting wings at supersonic speeds
- Non-lifting wings at supersonic speeds
- The design of warped wings with attached flow
- General properties of wings at low speeds
- Properties of vortex flows over slender wings
- Families of slender aircraft
- PROPERTIES AND DESIGN OF SLENDER AIRCRAFT. FOR SUPERSONIC FLIGHT
- Some problems of complete aircraft
- Some propulsion problems
- Some effects of non-uniform flows
- Interfering wings and ground effects
- Wing-fuselage interference
- The fuselage
- Some special designs
- Threedimensional wings
- Aerofoil section design
- THE DESIGN OF CLASSICAL AND SWEPT AIRCRAFT
- Swept wings in supersonic flow
- Swept wings in transonic flow
- High-lift effects
- Separation effects
- Properties of Classical and Swept Aircraft
- Viscosity effects
- Threedimensional sweep effects
- Previous Page
- An extension to swept-winged aircraft
- . The Aerodynamic Design of Aircraft
- PROPERTIES OF CLASSICAL AND SWEPT AIRCRAFT
- Elements of propulsion engines
- Propulsion flow cycles
- Overall thrust forces
- 3.4 Lifting bodies with shockwaves
- Slender wings with non-planar vortex wakes
- Wings with near-planar vortex wakes
- MEANS FOR GENERATING LIFT AND. PROPULSIVE FORCES
- THE TREATMENT OF AIRFLOWS
- The motivation of aviation
- An overall technical assessment
- PROLEGOMENA
- The Aerodynamic Design of Aircraft
- Category: The Art of the Helicopter