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UQx HYPERS301x 4.2.2 Mathematical Model of Flow with Friction
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0:30:51
UQx HYPERS301x 4.2.2 Mathematical Model of Flow with Friction
0:33:54
UQx Hypers301x 4.3.2v Mathmatical Model and Solution
0:17:24
UQx HYPERS301x 4.2.3 Interpretation of Results of Friction Model
0:12:45
UQx HYPERS301x 4.3.4v Stoichiometry
0:02:27
UQx Hypersonics
0:08:07
UQx Hypers301x 4.2.3.1 Flow Friction Example Problem
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UQx HYPERS301x 2.5.2 Isentropic Analysis
0:07:37
UQx Hypers301x 3.4.4 Losses Associated with Shockwaves - Entropy
0:08:09
UQx Hypers301x 2.4.2 Stagnation Temperature
0:14:49
UQx Hypers301x 1.6.5 Two Stage to Orbit
0:19:47
UQx HYPERS301x 5.3.2 Mach Number Independence-
0:19:29
UQx HYPERS301x 4.3.3 Interpretation of Results Heat Addition
0:10:27
UQx Hypers301x 1.6.2 Deriving the Rocket Equation
0:10:46
UQx Hypers301x 1.6.4 Single Stage to Orbit
0:16:41
UQx Hypers301x 3.4.2v2 Rankine Manipulations
0:06:28
UQx Hypers301x 2.3.4 The Perfect Gas
0:17:07
HYPERS301x 5.3.2 Dissociation
0:07:43
UQx Hypers301x 2.4.3 Stagnation Pressure
0:04:47
UQx Hypers301x 4.3.4.1 Stoichiometry Worked Example
0:15:48
UQx HYPERS301x 5.4.1 Hypersonic Equivalence Principle
0:02:32
UQx Hypers301x 2.5.1 Motivation
0:06:02
UQx HYPERS301x 1.2.1 Course Overview
0:09:44
UQx Hypers301x 6.5.1 Components
0:09:22
UQx Hypers301x 2.3.5 Isentropic Flow Relations
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