Aeronautical Science Group Assignment
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📅 2/2/2026
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Introduction to Aeronautical Science
Group members: Joshua, Phares, Mikiyas, Biruk, Abel
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Aircraft Selection
- Selected aircraft: CRJ100/200, CRJ700/705, CRJ900, CRJ1000, Global 5500
- All share similar configurations but vary in size and capacity
- Purpose: Compare performance metrics across different models
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Similarities and Differences
- Similarities: Regional jet design, turbofan engines, similar wing configurations
- Differences: Size, passenger capacity, range, and takeoff weight
- Focus on how size impacts performance metrics
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Range vs Takeoff Weight Graph
- Graph shows maximum range plotted against maximum takeoff weight
- Trend: Larger aircraft tend to have higher range and weight
- Notable outlier or exceptions in the trend
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Payload vs Takeoff Weight Graph
- Graph compares maximum payload weight with maximum takeoff weight
- Trend: Similar to range vs weight, but with specific variations
- Implications for airline operational efficiency
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New Airliner Requirements
- Requirement: 200 passengers and 3500 nmiles range
- Estimate maximum takeoff weight based on previous analysis
- Suggested aircraft model that fits these requirements
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Atmospheric Conditions at 22,000 ft
- Design requirement for jet fighter performance at high altitude
- Key atmospheric factors: Pressure (P), Temperature (T), Density (ρ)
- Standard values for calculations at 22,000 ft MSL
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Pressure Calculation Example
- Scenario: Airplane flying at 40 m/s at 2 km altitude
- Airflow velocity at wing point: 50 m/s
- Calculate pressure using inviscid, incompressible flow assumptions
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Key Findings
- Larger aircraft generally have greater range and payload capacity
- Specific trends in weight vs performance metrics
- Practical implications for aircraft selection and design
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Conclusion and Next Steps
- Summary of aircraft comparison and analysis
- Recommendations for airline requirements
- Future research directions in aeronautical science
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