NASA NTRS · 19920065248
Laminar hypersonic flow over a compression using the HANA code
Abstract
A hypersonic blunt-body code, HANA (Hypersonic Analysis for Aerobrakes), has been used to model the flow with compression corner angles of 15 and 24 degrees. A comparison is made between experimental flow data and numerical results of previous investigations which include surface pressures, skin friction coefficients, heat transfer rates, and flow field geometries.
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Fay, John F., Sambamurthi, Jay. 1992-07-01. Laminar hypersonic flow over a compression using the HANA code. https://ntrs.nasa.gov/citations/19920065248
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