Engineering > STUDY GUIDE > Embry-Riddle Aeronautical UniversityASCI 309Topic 4.3 Jet Performance. (All)
Embry-Riddle Aeronautical UniversityASCI 309Topic 4.3 Jet Performance.
Document Content and Description Below
Angle of Climb Start in your thrust and drag vs. airspeed plots Find the sine of the climb angle sinY = T – D / W (T) = Thrust (D) = Drag (W) = Weight Max rate of ... climb located where greatest distance between thrust available and thrust required is at. ** In a constant airspeed scenario, max angle will occur at the minimum drag condition [Show More]
Last updated: 3 years ago
Preview 1 out of 4 pages
Buy this document to get the full access instantly
Instant Download Access after purchase
Buy NowInstant download
We Accept:
Reviews( 0 )
$10.00
Can't find what you want? Try our AI powered Search
Document information
Connected school, study & course
About the document
Uploaded On
Aug 30, 2021
Number of pages
4
Written in
All
Additional information
This document has been written for:
Uploaded
Aug 30, 2021
Downloads
0
Views
88
.png)
