Question

Atmospheric pressure in kilo-pascals(KPa), P=f(h), is a function of the altitude h in feet, and decreases...

Atmospheric pressure in kilo-pascals(KPa), P=f(h), is a function of the altitude h in feet, and decreases as the altitude increases. The thrust T produced by an aircraft engine in pounds in a function of the pressure T=g(P).

a) Is f invertible? Explain your answer.

b) Interpret f(9,000)=70

c)Interpret g(f(8,000)).

D) Interpret (30,000)*g^-1=f(12,000).

Science   Advanced-Physics   
0 0
Add a commentTranscribed image text
Next >

Homework Answers

Answer #1

0 0
Know the answer?
Your Answer:

Post as a guest

Your Name:

What's your source?

Earn Coins

Coins can be redeemed for fabulous gifts.

Log In

Sign Up

Not the answer you're looking for?
Ask your own homework help question
Similar Questions
The atmospheric pressure, P, decreases exponentially with altitude, h. Suppose the air pressure is 101.3 kPa...
The atmospheric pressure, P, decreases exponentially with altitude, h. Suppose the air pressure is 101.3 kPa at sea level, and the air pressure at the peak of Mount Everest (altitude of 8848 m, the highest point on Earth) is 33.7 kPa. a. Find the rate of change of atmospheric pressure with respect to altitude at sea level. b. Find the air pressure on the surface of Dead Sea (altitude of 420 m below sea level, the lowest point on earth)....
The rate of change of atmospheric pressure P with respect to altitude h is proportional to...
The rate of change of atmospheric pressure P with respect to altitude h is proportional to P, provided that the temperature is constant. At a specific temperature, the pressure is 103.8 kPa at sea level and 89.3 kPa at h = 1,000 m. (Round your answers to one decimal place.) (a) What is the pressure at an altitude of 4500 m? (b) What is the pressure at the top of a mountain that is 6551 m high?
Atmospheric Pressure. The atmosphere in the lower stratosphere decreases exponentially from 473 lb/ft3 at 152 ft...
Atmospheric Pressure. The atmosphere in the lower stratosphere decreases exponentially from 473 lb/ft3 at 152 ft to 51 lb/ft2 at 82,345 ft. a) Find the exponnetial decay rate k, and write an equation for an equation for an exponential function that can be used to estimate the atmospheric preesure in the stratosphere h feet above 36,152 ft. b) Estimate the atmospheric pressure at 50,000 ft (h = 50,000 - 36,152). c) At what height is the atmosphere pressure 100 lb/ft2...
ADVERTISEMENT
Need Online Homework Help?

Get Answers For Free
Most questions answered within 1 hours.

Ask a Question
ADVERTISEMENT