Aircraft Performance
Material type: TextPublication details: New Delhi Wiley India 2007Description: 282pISBN:- 9788126537815
- 387.73 SAA-A
Item type | Current library | Collection | Call number | URL | Status | Date due | Barcode | |
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Reference Book | Amity Central Library ASET Aerospace | Reference | 387.73 SAA-A (Browse shelf(Opens below)) | Link to resource | Not For Loan | 22052 |
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358 Vayu Aerospace and Defence Review | 358 Vayu Aerospace and Defence Review | 358.407076 NAT-A AFCAT : Air Force Common Admission Test | 387.73 SAA-A Aircraft Performance | 500.5 SIN-E Elements of Space Physics | 516.0285 PRE-C Computational Geometry | 518 GER-A Applied Numerical Analysis |
1 The General Performance Problem.
1.1 Introduction.
1.2 Performance Characteristics.
1.3 The Approach.
2 Equations of Motion.
2.1 General Information.
2.2 The Energy Approach.
3 The Basics.
3.1 Fundamental Performance Equation.
3.2 Stalling Speed.
3.3 Maximum Velocity and Ceiling.
3.4 Gliding Flight.
4 Climbing Flight.
4.1 General.
4.2 Rate of Climb, Climb Angle.
4.3 Time to Climb.
4.4 Other Methods.
5 Range and Endurance.
5.1 Introduction.
5.2 Approximate, But Most Used, Methods.
5.3 Range Integration Method.
5.4 Other Considerations.
5.5 Endurance.
5.6 Additional Range and Endurance Topics.
6 Nonsteady Flight in the Vertical Plane.
6.1 Take-off and Landing.
6.2 Take-off Analysis.
6.3 Landing.
6.4 Accelerating Flight.
7 Maneuvering Flight.
7.1 Introduction.
7.2 Turns in Vertical Plane: Pull-Ups or Push-Overs.
7.3 V--n Diagram.
7.4 Turning Flight in Horizontal Plane.
7.5 Maximum Sustained Turning Performance.
7.6 The Maneuvering Diagram.
7.7 Spiral Flight.
8 Additional Topics.
8.1 Constraint Plot.
8.2 Energy Methods.
A Properties of Standard Atmosphere.
B On the Drag Coefficient.
C Selected Aircraft Data.
D Thrust Data for Performance Calculations.
E Some Useful Conversion Factors.
Index.
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