subject
Engineering, 16.01.2022 19:10 kedest

At a point in the test section of a supersonic wind tunnel, the pressure and density of the air are 1066 lb/ft2 and 1.23 × 10−3 slug/ft3, respectively. Calculate the temperature at this point. (Round the final answer to the nearest whole number.) The temperature at the given point is °R.

ansver
Answers: 1

Another question on Engineering

question
Engineering, 04.07.2019 18:10
What difference(s) did you notice using a pneumatic circuit over hydraulic circuit.explain why the pneumatic piston stumbles when it hits an obstacle.
Answers: 2
question
Engineering, 04.07.2019 18:10
During a steady flow process, the change of energy with respect to time is zero. a)- true b)- false
Answers: 2
question
Engineering, 04.07.2019 18:10
Afluid flows with a velocity field given by v=(x/t)i.. determine the local and convective accelerations when x=3 and t=1.
Answers: 2
question
Engineering, 04.07.2019 18:10
Shafts are machine elements that are used to a) carry axial loads b) direct shear loads c) transmit power d) rotate at constant speed e) none of the above circular and square shafts subjected to the same torque under the same circum behave a) the same way b) almost the same way
Answers: 2
You know the right answer?
At a point in the test section of a supersonic wind tunnel, the pressure and density of the air are...
Questions
question
Mathematics, 01.08.2021 21:40
question
Mathematics, 01.08.2021 21:40
question
Biology, 01.08.2021 21:40
question
Mathematics, 01.08.2021 21:40
question
Mathematics, 01.08.2021 21:40
question
Mathematics, 01.08.2021 21:40
Questions on the website: 13722359