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Airframe Structural Design notes
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Airframe Structural Design (ASD) pdf Lecture notes
Airframe Structural Design pdf Notes – ASD Notes Pdf file to download are listed below please check it
Complete Notes
1st Unit Airframe Structural Design Pdf Notes
2nd Unit Airframe Structural Design Pdf Notes
3rd Unit Airframe Structural Design Pdf Notes
4th Unit Airframe Structural Design Pdf Notes
5th Unit Airframe Structural Design Pdf Notes
Note: These notes are according to the R09 Syllabus book of JNTU. In R13 and R15, 8-units of R09 syllabus are combined into 5-units in R13 and R15 syllabus. If you have any doubts please refer to the JNTU Syllabus Book.
Topics covered
Unit-1:
- Structural design process
- planning, design
- construction
- philosophy of designing
- principal structural components of aircraf
- wings
- empennage
- landing gear
- the powerplant
- structural integrity and failure stiffness
- service life
- aerodynamic characteristics
- load analysis, flight loads, maneuver loads
- a structural design project may be divided into three phases, i.e. Planning, design and construction.
Unit-2:
- Wing loads
- Span-wise air load distribution
- Fuselage loads
- Aluminum alloys
- Titanium
- Plastics
- Composite materials
- Damage Tolerance
- The term damage tolerance as known today was traced during 15th century and Leonardo Da Vinci’s notebook on the design of flying machines.
Unit-3:
- Wing box
- Wing layout
- Wing Configuration
- Wing Structure
- Wing Spars ,Wing Ribs, Wing Skin
- Nacelles Nacelles
- FLIGHT CONTROL SURFACES
- A wing is a type of fin with a surface that produces aerodynamic forces facilitating movement through air and other gases, or water and other liquids.
- As such, wings have an airfoil shape
- a streamlined cross-sectional shape producing lift.
Unit-4:
- DESIGN OF FUSELAGE
- LANDING GEAR
- ENGINE MOUNTS Truss Type
- Monocoque Type
- Empennage
- Landing Gear
- Tail Wheel Gear Configuration
- Tricycle Gear
- The fuselage is the main structure or body of the fixed-wing aircraft.
- It provides space for cargo
- controls, accessories, passengers, and other equipment.
- In single-engine aircraft, the fuselage houses the power-plant.
Unit-5:
- FATIGUE LIFE
- DAMAGE TOLERANCE
- FAIL-SAFE DESIGN
- WEIGHT CONTROL AND BALANCE
- Common failure modes
- Damage Tolerance and Allowable Design & Limit Analysis
- Damage Tolerance and Allowable Design Limit Analysis
- Damage Tolerance
- Allowable Damage Limit (ADL)
- Fatigue Life Estimation Procedures For the Endurance of a Cardiac Valve
- Prosthesis: Stress/Life and Damage-Tolerant Analyses.
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