Summation of priorities of all objectives that need to be minimized Solution

STEP 0: Pre-Calculation Summary
Formula Used
Priority Sum of objectives to be minimized(%) = Cost Priority (%)+Weight Priority (%)+Period Priority (%)
Pmin = Pc+Pw+Pt
This formula uses 4 Variables
Variables Used
Priority Sum of objectives to be minimized(%) - Priority Sum of objectives to be minimized(%) is sum of all priority of objectives in all type of aircrafts mostly cost, weight and design period factors. Taken in percentage.
Cost Priority (%) - Cost Priority (%) is a factor which shows the priority of cost objective on a percentage scale. It is oriented according to the user's definition of priorities.
Weight Priority (%) - Weight Priority (%) is a factor which shows the priority of Weight factor on a percentage scale. It is oriented according to the user's definition of priorities.
Period Priority (%) - Period Priority (%) is a factor which shows the priority of Time factor of on a percentage scale. It is oriented according to the user's definition of priorities.
STEP 1: Convert Input(s) to Base Unit
Cost Priority (%): 10.11 --> No Conversion Required
Weight Priority (%): 15.1 --> No Conversion Required
Period Priority (%): 19 --> No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
Pmin = Pc+Pw+Pt --> 10.11+15.1+19
Evaluating ... ...
Pmin = 44.21
STEP 3: Convert Result to Output's Unit
44.21 --> No Conversion Required
FINAL ANSWER
44.21 <-- Priority Sum of objectives to be minimized(%)
(Calculation completed in 00.004 seconds)

Credits

Created by Vedant Chitte
All India Shri Shivaji Memorials Society's ,College of Engineering (AISSMS COE PUNE), Pune
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National Institute Of Technology (NIT), Hamirpur
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19 Design Process Calculators

Summations of priorities of objectives that need to be maximized (Millitary planes)
Go Priority Sum of objectives to be maximized (%) = Performance Priority (%)+Flight Quality Priority (%)+Scariness Priority (%)+Maintainability Priority (%)+Producibility Priority (%)+Disposability Priority (%)+Stealth Priority (%)
Thrust-to-Weight ratio given vertical velocity
Go Thrust-to-weight ratio = ((Vertical Airspeed/Aircraft Velocity)+((Dynamic Pressure/Wing Loading)*(Minimum Drag Coefficient))+((Lift Induced Drag Constant/Dynamic Pressure)*(Wing Loading)))
Priority of objective weight in design process given minimum design index
Go Weight Priority (%) = ((Minimum Design Index*100)-(Cost Index*Cost Priority (%))-(Period Index*Period Priority (%)))/Weight Index
Priority of objective cost in design process given minimum design index
Go Cost Priority (%) = ((Minimum Design Index*100)-(Weight Index*Weight Priority (%))-(Period Index*Period Priority (%)))/Cost Index
Priority of objective period of design given minimum design index
Go Period Priority (%) = ((Minimum Design Index*100)-(Weight Index*Weight Priority (%))-(Cost Index*Cost Priority (%)))/Period Index
Period of Design Index given Minimum Design Index
Go Period Index = ((Minimum Design Index*100)-(Weight Index*Weight Priority (%))-(Cost Index*Cost Priority (%)))/Period Priority (%)
Weight Index given Minimum Design Index
Go Weight Index = ((Minimum Design Index*100)-(Cost Index*Cost Priority (%))-(Period Index*Period Priority (%)))/Weight Priority (%)
Cost Index given Minimum Design Index
Go Cost Index = ((Minimum Design Index*100)-(Weight Index*Weight Priority (%))-(Period Index*Period Priority (%)))/Cost Priority (%)
Minimum design index
Go Minimum Design Index = ((Cost Index*Cost Priority (%))+(Weight Index*Weight Priority (%))+(Period Index*Period Priority (%)))/100
Battery Weight Fraction
Go Battery Weight Fraction = (Range of Aircraft/(Battery Specific Energy Capacity*3600*Efficiency*(1/[g])*Maximum Lift to Drag ratio of Aircraft))
Summation of priorities of all objectives that need to be minimized
Go Priority Sum of objectives to be minimized(%) = Cost Priority (%)+Weight Priority (%)+Period Priority (%)
Electric Power for Wind Turbine
Go Electric Power of Wind Turbine = Shaft Power*Efficiency of Generator*Efficiency of Transmission
Propulsion Net Thrust
Go Thrust force = Air Mass Flow Rate*(Velocity of Jet-Flight Velocity)
Maximum payload capability
Go Payload = Maximum take off weight-Operating empty weight-Fuel load
Induced Inflow Ratio in Hover
Go Inflow Ratio = Induced Velocity/(Rotor Radius*Angular Velocity)
Range increment of aircraft
Go Range increment of aircraft = Design range-Harmonic range
Mission fuel
Go Mission fuel = Fuel load-Reserve fuel
Reserve fuel
Go Reserve fuel = Fuel load-Mission fuel
Fuel load
Go Fuel load = Mission fuel+Reserve fuel

Summation of priorities of all objectives that need to be minimized Formula

Priority Sum of objectives to be minimized(%) = Cost Priority (%)+Weight Priority (%)+Period Priority (%)
Pmin = Pc+Pw+Pt

What are Priorities to be Minimized?

The Summation of the priorities of all objectives that need to be minimized formula is defined as the summation of the Priority Percentages that need to be minimized in the model of aircraft concept.

How to Calculate Summation of priorities of all objectives that need to be minimized?

Summation of priorities of all objectives that need to be minimized calculator uses Priority Sum of objectives to be minimized(%) = Cost Priority (%)+Weight Priority (%)+Period Priority (%) to calculate the Priority Sum of objectives to be minimized(%), The Summation of priorities of all objectives that need to be minimized formula used to calculate the overall priority of objectives that need to be minimized in military aircraft design, this approach helps prioritize design decisions and resource allocations to minimize vulnerabilities and enhance overall aircraft performance. Priority Sum of objectives to be minimized(%) is denoted by Pmin symbol.

How to calculate Summation of priorities of all objectives that need to be minimized using this online calculator? To use this online calculator for Summation of priorities of all objectives that need to be minimized, enter Cost Priority (%) (Pc), Weight Priority (%) (Pw) & Period Priority (%) (Pt) and hit the calculate button. Here is how the Summation of priorities of all objectives that need to be minimized calculation can be explained with given input values -> 44.21 = 10.11+15.1+19.

FAQ

What is Summation of priorities of all objectives that need to be minimized?
The Summation of priorities of all objectives that need to be minimized formula used to calculate the overall priority of objectives that need to be minimized in military aircraft design, this approach helps prioritize design decisions and resource allocations to minimize vulnerabilities and enhance overall aircraft performance and is represented as Pmin = Pc+Pw+Pt or Priority Sum of objectives to be minimized(%) = Cost Priority (%)+Weight Priority (%)+Period Priority (%). Cost Priority (%) is a factor which shows the priority of cost objective on a percentage scale. It is oriented according to the user's definition of priorities, Weight Priority (%) is a factor which shows the priority of Weight factor on a percentage scale. It is oriented according to the user's definition of priorities & Period Priority (%) is a factor which shows the priority of Time factor of on a percentage scale. It is oriented according to the user's definition of priorities.
How to calculate Summation of priorities of all objectives that need to be minimized?
The Summation of priorities of all objectives that need to be minimized formula used to calculate the overall priority of objectives that need to be minimized in military aircraft design, this approach helps prioritize design decisions and resource allocations to minimize vulnerabilities and enhance overall aircraft performance is calculated using Priority Sum of objectives to be minimized(%) = Cost Priority (%)+Weight Priority (%)+Period Priority (%). To calculate Summation of priorities of all objectives that need to be minimized, you need Cost Priority (%) (Pc), Weight Priority (%) (Pw) & Period Priority (%) (Pt). With our tool, you need to enter the respective value for Cost Priority (%), Weight Priority (%) & Period Priority (%) and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
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