FormulaDen logo
FormulaDen.com
Search
Physics Chemistry Math Chemical Engineering Civil Electrical Electronics Electronics and Instrumentation Materials Science Mechanical Production Engineering Financial Health
Fx Copy
LaTeX Copy
Drag Coefficient is a dimensionless quantity that is used to quantify the drag or resistance of an object in a fluid environment, such as air or water. Check FAQs
CD=CL⋅TW
CD - Drag Coefficient?CL - Lift Coefficient?TW - Thrust-to-Weight Ratio?

Coefficient of Drag for given Thrust-to-Weight Ratio Example

With values
With units
Only example

Here is how the Coefficient of Drag for given Thrust-to-Weight Ratio equation looks like with Values.

Here is how the Coefficient of Drag for given Thrust-to-Weight Ratio equation looks like with Units.

Here is how the Coefficient of Drag for given Thrust-to-Weight Ratio equation looks like.

0.495Edit=1.1Edit⋅0.45Edit
Solution
Copy
Reset
Share
You are here -
HomeIcon Home » Category Physics » Category Aerospace » Category Aircraft Mechanics » fx Coefficient of Drag for given Thrust-to-Weight Ratio

Coefficient of Drag for given Thrust-to-Weight Ratio Solution

Follow our step by step solution on how to calculate Coefficient of Drag for given Thrust-to-Weight Ratio?

FIRST Step Consider the formula
CD=CL⋅TW
Next Step Substitute values of Variables
∴ CD=1.1⋅0.45
Next Step Prepare to Evaluate
∴ CD=1.1⋅0.45
LAST Step Evaluate
∴CD=0.495

Coefficient of Drag for given Thrust-to-Weight Ratio Formula Elements

Variables
Drag Coefficient
Drag Coefficient is a dimensionless quantity that is used to quantify the drag or resistance of an object in a fluid environment, such as air or water.
Symbol: CD
Measurement: NAUnit: Unitless
Note: Value can be positive or negative.
Formulas to find Drag CoefficientOpen Variable
Lift Coefficient
The Lift Coefficient is a dimensionless coefficient that relates the lift generated by a lifting body to the fluid density around the body, the fluid velocity and an associated reference area.
Symbol: CL
Measurement: NAUnit: Unitless
Note: Value should be greater than 0.
Formulas to find Lift CoefficientOpen Variable
Thrust-to-Weight Ratio
Thrust-to-Weight Ratio is a dimensionless ratio of thrust to weight of a rocket, jet engine, propeller engine.
Symbol: TW
Measurement: NAUnit: Unitless
Note: Value should be greater than 0.
Formulas to find Thrust-to-Weight RatioOpen Variable

Credits

Creator Image
Created by Vinay Mishra LinkedIn Logo
Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune
Vinay Mishra has created this Formula and 300+ more formulas!
Verifier Image
Verified by Sai Venkata Phanindra Chary Arendra LinkedIn Logo
Vallurupalli Nageswara Rao Vignana Jyothi Institute of Engineering and Technology (VNRVJIET), Hyderabad
Sai Venkata Phanindra Chary Arendra has verified this Formula and 300+ more formulas!

Other Formulas to find Drag Coefficient

​Go Coefficient of Drag for given Thrust and Weight
CD=T⋅CLWbody

Other formulas in Lift and Drag Requirements category

​Go Drag for Level and Unaccelerated Flight
FD=T⋅cos(σT)
​Go Lift for Unaccelerated Flight
FL=Wbody-T⋅sin(σT)
​Go Drag for Level and Unaccelerated Flight at Negligible Thrust Angle
FD=Pdynamic⋅A⋅CD
​Go Lift for Level and Unaccelerated Flight at Negligible Thrust Angle
FL=Pdynamic⋅A⋅CL

How to Evaluate Coefficient of Drag for given Thrust-to-Weight Ratio?

Coefficient of Drag for given Thrust-to-Weight Ratio evaluator uses Drag Coefficient = Lift Coefficient*Thrust-to-Weight Ratio to evaluate the Drag Coefficient, The Coefficient of Drag for given Thrust-to-Weight Ratio suggests that the drag coefficient is directly proportional to both the lift coefficient and the thrust-to-weight ratio, this implies that as the lift coefficient or thrust-to-weight ratio increases, the drag coefficient also increases proportionally. Drag Coefficient is denoted by CD symbol.

How to evaluate Coefficient of Drag for given Thrust-to-Weight Ratio using this online evaluator? To use this online evaluator for Coefficient of Drag for given Thrust-to-Weight Ratio, enter Lift Coefficient (CL) & Thrust-to-Weight Ratio (TW) and hit the calculate button.

FAQs on Coefficient of Drag for given Thrust-to-Weight Ratio

What is the formula to find Coefficient of Drag for given Thrust-to-Weight Ratio?
The formula of Coefficient of Drag for given Thrust-to-Weight Ratio is expressed as Drag Coefficient = Lift Coefficient*Thrust-to-Weight Ratio. Here is an example- 66 = 1.1*0.45.
How to calculate Coefficient of Drag for given Thrust-to-Weight Ratio?
With Lift Coefficient (CL) & Thrust-to-Weight Ratio (TW) we can find Coefficient of Drag for given Thrust-to-Weight Ratio using the formula - Drag Coefficient = Lift Coefficient*Thrust-to-Weight Ratio.
What are the other ways to Calculate Drag Coefficient?
Here are the different ways to Calculate Drag Coefficient-
  • Drag Coefficient=(Thrust*Lift Coefficient)/Weight of BodyOpenImg
© 2024-2025. Developed & Maintained by softUsvista Inc.
Copied!