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Predicted Shock Envelopes about Two Types of Vehicles at Large Angles of Attack (1961)

Kaattari, George E.

In: CASI

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Publication Date: 2019-08-15

Description: Methods based on oblique - and normal-shock relationships and the continuity of mass flow through suitably chosen volume elements between the shock and body were developed t o predict shock envelopes about two types of vehicles being considered for atmosphere entry. One type is a high-drag capsule shape. The other type is essentially a slender tri- angular wing capable of providing high lift or high drag, depending on the angle of attack. Predicted and measured shock envelopes were compared f o Mach number range of 3 to 15 for vehicles at high angles of attack; good agreement was found. Most of the available experimental data were in a speed and temperature range in which no important real-gas effects occurred.

Keywords: Spacecraft Design, Testing and Performance

Type: NASA-TN-D-860 , A-491

Format: application/pdf

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