Airplane Aircraft Wing Lift Design Equations Formulas Calculator

Home Page 2 Page 3 Page 4 Page 5 Physics Math Fluid Mechanics Investment Finance Loan Calculator Nursing Math Jobs Salary

Solving For Lift Force

Inputs:

Conversions:

coefficient of lift (C_L)	=	=
density (p)	=	=	kilogram/meter^3
velocity (V)	=	=	meter/second
surface area (A)	=	=	meter^2

Solution:

lift force (L)

HAS NOT BEEN CALCULATED

Other Units:

Change Equation
Select an equation to solve for a different unknown

Aircraft and airplane wing lift equations

	Solve for lift force
	Solve for lift coefficient
	Solve for air density
	Solve for velocity
	Solve for lift surface area

Where

L	=	lift force
C_L	=	lift coefficient
p	=	air density
V	=	velocity
A	=	lift surface area

Reference - Books:

1) Munson, B.R., D. F. Young, and T. H. Okiishi. 1994. Fundamentals of Fluid Mechanics. John Wiley and Sons, Inc. 2nd ed.

AJ Design - Online Science Mathematics Engineering Software Programs | 2 | 3 | 4 | 5

by Jimmy Raymond

Add to circles to follow new app, calculator, bug report and request updates from AJ Design.

Technical Tools, Specifications, How to Guides, Training, Applications, Examples, Tutorials, Reviews, Answers, Test Review Resources, Analysis, Homework Solutions, Help, Data and Information for Engineers, Technicians, Teachers, Tutors, Researchers, K-12 Education, College and High School Students, Science Fair Projects and Scientists

Contact: aj@ajdesigner.com