Design of Business Jet Aircraft (AINAS)

This proposal presents a supersonic business jet that represents a new generation of corporate aviation, one that embraces new technology with a fresh design that allows for luxury, efficiency, and premium performance. This business jet is specifically designed for experienced executives and high-net-worth individuals who increasingly expect a quiet, comfortable, and productive travel experience for either business or leisure travel. The definition of a next-generation supersonic business jet relies on several characteristics of the design, including: Low wing swept-wing configuration, which provides stability in high-speed situations and is typical for high-speed aircraft such as the F-15 jets. By having the engines mounted above the wings and the fuselage, we can reduce cabin noise as well as provide better control of the aircraft. The T-tail configuration helps with thrust vectoring and increases the performance of the design in all phases of flight. Many priorities have been considered, including fuel efficiency, range, and cabin comfort. The jet allows for first-class service and still adheres to utmost safety and comfort that every rigorous and modern aerodynamic and structural principles.

Keywords: Supersonic business jet, Aircraft conceptual design, Thrust vectoring, Payload and range analysis, Wing and fuselage optimization, NACA 64A010 airfoil, Sustainable aviation fuel (SAF), V-n diagram, Luxury executive travel, Noise and drag reduction.

List of Contents…………….

Chapter 1: Introduction to Aircraft Design

1.1 Introduction

1.2 Aircraft Design Process

Chapter 2: Introduction To Business Jet (AINAS)

2.1 Introduction to Business Jets

2.2 AINAS Business Jet

2.3 Mission profile

Chapter 3: Conceptual Sketch

3.1Dimension

3.2key features

Chapter 4: Take-Off Weight Estimation

4.1 Introduction and Formulation

4.2 Take-off weight estimation

Chapter 5: Payload And Range Sizing

5.1 Payload Sizing

5.2 Range Sizing

Chapter 6: Airfoil Selection

6.1 Role of Airfoil in Aircraft Design

6.2 The Airfoil Selection for AINAS

6.3 Study of Airfoil Characteristics

Chapter 7: Wing Design

7.1 Key parameters

7.2 Wing area

7.3 Wing loading

7.4 Aspect ratio

7.5 Sweep

Chapter 8: Fuselage Design

8.1 Key Factors in Fuselage Design

8.2 Major Fuselage Design Parameters

8.3 Types of Fuselage Construction

8.4 Aerodynamic Considerations

Chapter 9: Landing Gear Design

Chapter 10: Thrust Required

Chapter 11: Drag Estimation

Chapter 12: V-N Diagram

Chapter 13: Cost Estimation

Chapter 14: Design Conclusion

Appendix

References