q6_19 - and stagnation temperatures are the same, since the...

Info iconThis preview shows pages 1–3. Sign up to view the full content.

View Full Document Right Arrow Icon
Background image of page 1

Info iconThis preview has intentionally blurred sections. Sign up to view the full version.

View Full DocumentRight Arrow Icon
Chapter 6 Question 19 Answer: (1) T T1 = T 1 > T atm The flow stagnates on a moving body (the spinning fan blade). Thus the scenario is similar to a supersonic aircraft flying through the atmosphere. The stagnation temperature is elevated above the static temperature of the atmosphere. On the blade itself, the static
Background image of page 2
Background image of page 3
This is the end of the preview. Sign up to access the rest of the document.

Unformatted text preview: and stagnation temperatures are the same, since the flow is not moving relative to the blade. Class Response (2003): Class Response (2002):...
View Full Document

This note was uploaded on 01/28/2012 for the course AERO 16.01 taught by Professor Markdrela during the Fall '05 term at MIT.

Page1 / 3

q6_19 - and stagnation temperatures are the same, since the...

This preview shows document pages 1 - 3. Sign up to view the full document.

View Full Document Right Arrow Icon
Ask a homework question - tutors are online