MIT 16.885J / ESD.35J Aircraft Systems Engineering - Fall 2005

Lecture 12: Aerothermodynamics

author:Bob Ried
published: Nov. 4, 2009, recorded: October 2005, views: 35

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Slides

Slides
53:43	Entry Flight Regimes: Apollo and Orbiter
64:25	Design and Flight Test Environments
72:19	Design Heating Methodology
76:23	Logic for Predicting Boundary Layer Transition on the Orbiter
78:48	Surface Catalysis Flight Prediction Process
90:40	Orbiter Flow Field Results
92:02	Comparison of STS-3 Flight Data with Preflight Test Predictions: Forward Windward Centerline
97:30	Comparison of STS-3 Flight Data with Preflight Test Predictions: Midbody Windward Centerline
99:08	Comparison of STS-3 Flight Data with Preflight Test Predictions: Aft Windward Centerline
99:56	STS-3, Orbiter Inferred and Predicted Heat Flux
102:22	Leeward Surface Flight Data vs. Reynolds Number
104:18	SA 201
106:07	Entry Bondline Thermal Response, Midbody Windward
111:23	Matrix of Understanding

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