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Jet Sense : The Philosophy and the Art of Jet Transport Design / Zarir D. Pastakia.
- Format:
- Book
- Author/Creator:
- Pastakia, Zarir D., author.
- Language:
- English
- Subjects (All):
- Aeronautics, Commercial.
- Jet transports--Design and construction.
- Jet transports.
- Physical Description:
- 1 online resource (265 pages)
- Edition:
- First edition.
- Place of Publication:
- Warrendale, PA : SAE International, [2024]
- Summary:
- Jet Sense: The Philosophy and the Art of Jet Transport Design by Zarir D. Pastakia provides an in-depth exploration of the principles and methodologies involved in the design of jet transport aircraft. Drawing on over 23 years of experience in the field, Pastakia shares insights into the intricate balance between art and science in aircraft design, focusing on aspects such as wing design, fuselage layout, and propulsion systems. The book is intended for aviation enthusiasts, pilots, aerospace professionals, and anyone interested in understanding the complex factors that influence the design and performance of commercial aircraft. It offers a unique perspective on both the philosophical and practical approaches to jet transport design, incorporating novel methods and industry practices. Generated by AI.
- Contents:
- Front Cover
- Title Page
- Copyright Page
- Contents
- Preface
- Foreword
- Acknowledgements
- Chapter 1: Markets and Requirements
- Chapter 2: Aircraft Sizing
- Speed of Sound
- Cruise Speed
- Thrust-Specific Fuel Consumption
- Lift-to-Drag Ratio
- Profile Drag
- Altitude Effects Related to Profile Drag
- Induced Drag or Lift-Dependent Drag
- Compressibility Drag
- The Weight Ratio
- The Aircraft Sizing Process
- The Mission
- Design Mission
- Alternate or Reserve Mission
- Define the Fuselage Cross Section
- Double-Deck and One-and-Half-Deck Aircraft
- Engine Selection
- Wing Sizing
- Wing Sweep
- High Sweep
- Thickness-to-Chord Ratio (t/c)
- High t/c
- Low t/c
- Aspect Ratio
- Taper Ratio
- Maximum Lift Coefficient
- Selecting the Wing Area
- Design Weights
- The Initial and Optimum Cruise Altitude at MTOW
- High-Lift Devices
- High-Lift Devices and the Lift Curve Slope
- Thrust Sizing
- Take-Off Thrust Sizing
- Second Segment Climb Thrust Sizing
- Top of Climb Thrust Sizing
- Fuel Volume
- Limitations of the Sizing Method and Optimization
- Operating Cost
- Airplane Price
- Utilization
- Flight Crew Expenses
- Fuel and Oil Expenses
- Insurance Expenses
- Other Flying Operation Expenses
- Passenger Service Expenses (PSE)
- Flight Equipment Maintenance Expenses
- Flight Equipment Depreciation and Amortization Expenses
- Landing Fees
- Total Aircraft Operating Cost
- Configuring the Airplane
- Chapter 3: Fuselage Cross-Section Design
- Cross Sections of Existing Jet Transports
- Chapter 4: Fuselage Layout
- Developing the Fuselage Plan View
- Developing the Fuselage Side View
- AC 25.773-1: Criteria for Pilot Compartment Visibility
- Landing Vision
- Obstructions to Vision.
- Chapter 5: Cabin Layout and Door Positioning
- Understanding the Rules and the Terminology
- Passenger Cabin Length
- Passenger Zones or Zones
- Exit Rating
- Exit Unit
- Fuselage Length Factor
- Exit Offset
- Individual Zone Passenger Capacity
- Sequential Zone Passenger Capacity
- Terminal Servicing and Other Considerations
- Chapter 6: Wing and Landing Gear Layout
- Common Wing Terminology
- Thickness-to-Chord Ratio
- Dihedral
- Mean Aerodynamic Chord (MAC)
- ESDU Wing Area
- Define the ESDU Planform
- Wing Integration
- Landing Gear and Wheel Well Sizing
- Main Landing Gear
- Nose Landing Gear
- Wing Structure Considerations
- Paying Attention to the Aerodynamics
- The Process Steps
- Chapter 7: Layout of the Horizontal Tail
- Definitions
- Tail Volume Coefficient
- Reference Horizontal Tail Information
- Thickness-to-Chord Ratio and Quarter-Chord Sweep
- Center of Gravity
- Ice Protection
- Relaxed Stability
- Horizontal Tail Fuel Tank
- Chapter 8: Vertical Tail Layout
- The Vertical Tail Volume Coefficient
- Sizing the Vertical Tail for Aircraft with Aft Fuselage-Mounted Engines
- Chapter 9: Propulsion and the Jet Engine
- The Jet Engine
- Figures of Merit for Engine Choice
- The Inlet
- The Fan and Compressor
- The Combustion Chamber
- The Turbine
- The Nozzle
- Engine Installation
- Wing-Mounted Location
- Aft Fuselage-Mounted Location
- Chapter 10: Pulling It All Together
- Locate the Wing in Plan View [ 73 , 74 , 78 ]
- Locate the Horizontal Tail or Stabilizer in Plan View [ 73 , 74 , 78 ]
- Locate the Wing in Side View [ 73 , 74 , 78 ]
- Locate the Empennage in Side View [ 73 , 74 , 78 ]
- Other Considerations.
- The General Arrangement or 3-View
- References
- Aircraft Sizing and Design
- Fuselage Design
- Wing Design
- Empennage Design
- Propulsion
- Aircraft Performance
- Economics
- Other
- Appendix A: The Standard Atmosphere
- Appendix B: Different Approaches to the Same Requirement. There Is No Substitute for Creativity and Imagination
- Specification B35/46-Summary of Aircraft Requirements [ 65 , 80 ]
- Appendix C: Rapid Estimating Methods
- Effect of Aspect Ratio on the Drag Polar
- Propulsion Scaling [ 60 ]
- Appendix D: Data on Existing Jet Transports
- Embraer 190-E2 Jet
- Airbus A321neo-XLR
- Airbus A330-300
- Boeing 787-9 Dreamliner
- A350-900 XWB
- Boeing 777-300ER
- Boeing (McDonnell Douglas) MD-11
- Boeing 747-8 Intercontinental
- Airbus A380
- Appendix E: Environmental Factors
- Noise [76, 77]
- Wake Vortex
- Separations and the ICAO Rules [85]
- Emissions
- The 2028 ICAO CO 2 Standard [77, 84]
- Appendix F: Freighters
- Key Vocabulary for Freighter Aircraft
- New Build Freighter
- Converted Freighter
- Revenue Payload
- Gross Structural Payload
- Cargo Volume
- Cargo Density
- Volumetric Payload
- Unit Load Device or ULD
- Pallet
- Container
- Tare Weight
- Cargo Handling System or CHS
- General Market Freighter
- Package Freighter
- Freight Aircraft Considerations
- Quick Rules of Thumb
- A Promising Future for Air Cargo and Freighter Transports
- Index
- About the Author
- Back Cover.
- Notes:
- Description based on publisher supplied metadata and other sources.
- Part of the metadata in this record was created by AI, based on the text of the resource.
- Description based on print version record.
- Includes bibliographical references and index.
- ISBN:
- 9781468606010
- 1468606018
- 9781468606003
- 146860600X
- OCLC:
- 1422169080
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