Get 2 FREE Instant-Explanations on Filo with code FILOAPP

In a test experiment on a model aeroplane in a wind tunnel, th

Question

In a test experiment on a model aeroplane in a wind tunnel, the flow speeds on the upper and lower surfaces of the wing are $70 m s^{- 1}$ and $83 m s^{- 1}$ respectively. What is the lift on the wing, if its area is $2.5 m^{2} ?$ Take the density of air to be $1.3 k g m^{- 3}$

Name: Video solution 1: In a test experiment on a model aeroplane in a wind tunnel, the flow speeds on the upper and lower surfaces of the wing are 70ms−1 and 83ms−1 respectively. What is the lift on the wing, if its area is 2.5m2? Take the density of air to be 1.3kgm−3
Uploaded: 2021-01-01T18:41:02.000Z
Duration: 2 min
Description: Video solution 1: In a test experiment on a model aeroplane in a wind tunnel, the flow speeds on the upper and lower surfaces of the wing are 70ms−1 and 83ms−1 respectively. What is the lift on the wing, if its area is 2.5m2? Take the density of air to be 1.3kgm−3

1513 N

1513 dines

151.3 N

151.3 dynes

Views: 1,005 students

Found 6 tutors discussing this question

Sebastian Discussed

In a test experiment on a model aeroplane in a wind tunnel, the flow speeds on the upper and lower surfaces of the wing are

70 m s^{- 1}

and

83 m s^{- 1}

respectively. What is the lift on the wing, if its area is

2.5 m^{2} ?

Take the density of air to be

1.3 k g m^{- 3}

12 mins ago

Discuss this question LIVE

12 mins ago

Filo tutor solutions (1)

Learn from their 1-to-1 discussion with Filo tutors.

Ask your question, on a video call with tutor

Connect instantly with this tutor

Connect now

Was this solution helpful?

150

Report

One destination for complete JEE/NEET preparation

One destination to cover all your homework and assignment needs

Learn Practice Revision Succeed

Instant 1:1 help, 24x7

60, 000+ Expert tutors

Textbook solutions

Big idea maths, McGraw-Hill Education etc

Essay review

Get expert feedback on your essay

Schedule classes

High dosage tutoring from Dedicated 3 experts

Trusted by 4 million+ students

Stuck on the question or explanation?

Connect with our physics tutors online and get step by step solution of this question.

231 students are taking LIVE classes

Question Text	In a test experiment on a model aeroplane in a wind tunnel, the flow speeds on the upper and lower surfaces of the wing are $70 m s^{- 1}$ and $83 m s^{- 1}$ respectively. What is the lift on the wing, if its area is $2.5 m^{2} ?$ Take the density of air to be $1.3 k g m^{- 3}$
Answer Type	Video solution: 1
Upvotes	150

In a test experiment on a model aeroplane in a wind tunnel, the flow speeds on the upper and lower surfaces of the wing are 70ms−1 and 83ms−1 respectively. What is the lift on the wing, if its area is 2.5m2? Take the density of air to be 1.3kgm−3

Filo tutor solutions (1)

Practice questions from similar books

In a test experiment on a model aeroplane in a wind tunnel, the flow speeds on the upper and lower surfaces of the wing are $70 m s^{- 1}$ and $83 m s^{- 1}$ respectively. What is the lift on the wing, if its area is $2.5 m^{2} ?$ Take the density of air to be $1.3 k g m^{- 3}$