Saarlas, Maido
Aircraft performance Maido Saarlas - [1st?] ed. - Hoboken John Wiley - xiv, 282 p. gráficos
Apéndices e índice alfabético, al final del libro
Indice Alfabético The general performance problem : Introduction.
Performance Characteristics.
Absolute Performance Characteristics. Functional Performance Characteristics.
The approach Equations of motion : General Information. The Energy Approach
The basics : Fundamental Performance Equation.
Stalling Speed.
Maximun Velocity and Ceiling. General Considerations. Drag and Drag Polar. Flight Envelope: Vmax V min. Power Required and power Available. Turboprop Engines.
Gliding Flight. Glide Angle and SInking Speed. Gilde Range and Endurance
Climbing flight . General. Rate of Climb, Climb Angle. Time to Climb. Other Methods. Shallow Flight Paths.Load Factor n =/ 1*.
Partial Power and Excess Power. Considerations.
TurbojetsRange and endurance : Introduction. Approximate, But Most Used, Methods. Reciprocating Engine. Jet Aircraft.
Range Integration Methods. Basic Methodology. An Operationa Approach.
Other Considerations. Flight Speeds. Effect of Energy Change on Range.
Endurance. Reciprocating Engines. Turbojets. Endurance Integration Method. Additional Range and Endurance Topics. The Effect of Wind. Some Range and Endurance Comparisons Nonsteady flight in the vertical plane : Take-off and Landing.Take-off Analysis.Ground Run. Rotation Distance. Transition Distance. Take-off Time. Factors Influencing the Take-off. Landing. Landing Phases. Landing Run. The Approach Distance. The Flare Distance. Accelerating Flight
Maneuvering flight : Introducción. Turns in Vertical Plane: Pull-Ups or Push-Overs. V-n Diagram.
Turning Flight in Horizontal Plane. Maximun Sustained Turning Performamce. Maximun Load factor. Minimum Turn Radius. The Maneuvering Diagram. Spiral Flight. Additional topics : Constraint Plot. Take-off and Landing. Constraints Tied to Performance Equation. Energy Methods
10: 0-470-04416-0 13: 978-0-470-04416-2
INGENIERIA AERONAUTICA PROYECTO Y DISENO AERODINAMICO
Aircraft performance Maido Saarlas - [1st?] ed. - Hoboken John Wiley - xiv, 282 p. gráficos
Apéndices e índice alfabético, al final del libro
Indice Alfabético The general performance problem : Introduction.
Performance Characteristics.
Absolute Performance Characteristics. Functional Performance Characteristics.
The approach Equations of motion : General Information. The Energy Approach
The basics : Fundamental Performance Equation.
Stalling Speed.
Maximun Velocity and Ceiling. General Considerations. Drag and Drag Polar. Flight Envelope: Vmax V min. Power Required and power Available. Turboprop Engines.
Gliding Flight. Glide Angle and SInking Speed. Gilde Range and Endurance
Climbing flight . General. Rate of Climb, Climb Angle. Time to Climb. Other Methods. Shallow Flight Paths.Load Factor n =/ 1*.
Partial Power and Excess Power. Considerations.
TurbojetsRange and endurance : Introduction. Approximate, But Most Used, Methods. Reciprocating Engine. Jet Aircraft.
Range Integration Methods. Basic Methodology. An Operationa Approach.
Other Considerations. Flight Speeds. Effect of Energy Change on Range.
Endurance. Reciprocating Engines. Turbojets. Endurance Integration Method. Additional Range and Endurance Topics. The Effect of Wind. Some Range and Endurance Comparisons Nonsteady flight in the vertical plane : Take-off and Landing.Take-off Analysis.Ground Run. Rotation Distance. Transition Distance. Take-off Time. Factors Influencing the Take-off. Landing. Landing Phases. Landing Run. The Approach Distance. The Flare Distance. Accelerating Flight
Maneuvering flight : Introducción. Turns in Vertical Plane: Pull-Ups or Push-Overs. V-n Diagram.
Turning Flight in Horizontal Plane. Maximun Sustained Turning Performamce. Maximun Load factor. Minimum Turn Radius. The Maneuvering Diagram. Spiral Flight. Additional topics : Constraint Plot. Take-off and Landing. Constraints Tied to Performance Equation. Energy Methods
10: 0-470-04416-0 13: 978-0-470-04416-2
INGENIERIA AERONAUTICA PROYECTO Y DISENO AERODINAMICO