Calculators Created by Vedant Chitte

All India Shri Shivaji Memorials Society's ,College of Engineering (AISSMS COE PUNE), Pune
42
Formulas Created
4
Formulas Verified
5
Across Categories

List of Calculators by Vedant Chitte

Following is a combined list of all the calculators that have been created and verified by Vedant Chitte. Vedant Chitte has created 42 and verified 4 calculators across 5 different categories till date.
Created Cost index in terms of minimum design index
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Created Minimum design index
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Created Period of design index in terms of minimum design index
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Created Priority of objective cost in design process given minimum design index
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Created Priority of objective period of design given minimum design index
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Created Priority of objective weight in design process given minimum design index
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Created Summation of priorities of all objectives that need to be minimized
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Created Summations of priorities of objectives that need to be maximized (Millitary planes)
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Created Weight index in terms of minimum design index
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5 More Aircraft Conceptual Design Calculators
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Created Crew Weight in terms of Fuel and Empty Weight Fraction
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Created Crew Weight in terms of Takeoff Weight
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Created Cruise Weight Fraction for Jet Aircraft
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Created Cruise Weight Fraction for Prop-Driven Aircraft
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Created Empty Weight Fraction
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Created Empty Weight Fraction in terms of Takeoff Weight and Fuel Fraction
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Created Empty Weight in terms of Empty Weight Fraction
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Created Empty Weight in terms of Takeoff Weight
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Created Fuel Fraction
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Created Fuel Fraction in terms of Takeoff Weight and Empty Weight Fraction
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Created Fuel Weight in terms of Fuel Fraction
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Created Fuel Weight in terms of Takeoff Weight
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Created Lift to Drag for maximum Endurance in terms of Preliminary Endurance for Prop-Driven Aircraft
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Created Maximum Lift to Drag Ratio in terms of Preliminary Endurance for Jet Aircraft
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Created Maximum Lift to Drag Ratio in terms of Range for Jet Aircraft
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Created Maximum Lift to Drag Ratio in terms of Range for Prop-driven Aircraft
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Created Optimum Range for Jet Aircraft in Cruising Phase
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Created Optimum Range for Prop-Driven Aircraft in Cruising Phase
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Created Payload Weight in terms of Fuel and Empty Weight Fractions
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Created Payload Weight in terms of Takeoff Weight
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Created Preliminary Endurance for Jet Aircraft
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Created Preliminary endurance for Prop-Driven Aircraft
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Created Preliminary Take Off Weight Built-up for manned aircraft
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Created Preliminary Take off Weight Built-up for manned aircraft in terms of fuel and empty weight fraction
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Created Propeller Efficiency in terms of Preliminary Endurance for Prop-Driven Aircraft
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Created Propeller Efficiency in terms of Range for Prop-Driven Aircraft
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Created Specific Fuel Consumption in terms of Preliminary Endurance for Jet Aircraft
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Created Specific Fuel Consumption in terms of Preliminary Endurance for Prop-Driven Aircraft
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Created Specific Fuel Consumption in terms of Range for Jet Aircraft
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Created Specific Fuel Consumption in terms of Range for Prop-Driven Aircraft
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Created Takeoff Weight in terms of Empty Weight Fraction
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Created Takeoff Weight in terms of Fuel Fraction
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Created Velocity for Maximizing Range in terms of Range for Jet Aircraft
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5 More Aircraft Preliminary Weight Built Up Calculators
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Verified Mean Effective Pressure in Otto Cycle
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8 More Air-Standard Cycles Calculators
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Verified Geometric step ratio
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Verified Range ratio in preferred Series
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11 More Machine Design Calculators
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Verified Wheel rate in vehicle
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11 More Race Car Vehicle Dynamics Calculators
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