Lecture Notes
Lecture 6
Description:
This resource contains information regarding modeling of thermal rocket engines; nozzle flow; control of mass flow.
Resource Type:
Lecture Notes
pdf
945 kB
Lecture 6
Course Info
Instructor
Departments
As Taught In
Spring
2012
Level
Learning Resource Types
assignment_turned_in
Problem Sets with Solutions
grading
Exams with Solutions
notes
Lecture Notes