Actions for Subsonic aerodynamic heat transfer to a surface recessed within a forward stagnation region slit

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Subsonic aerodynamic heat transfer to a surface recessed within a forward stagnation region slit

Author
Scott, S. J.
Published
Dec 1, 1963.
Physical Description
1 electronic document
Online Version

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Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
Heat transfer to surface recessed within forward stagnation region slit under subsonic arc jet conditions
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19640001990.
Accession ID: 64N11899.
NASA-TN-D-2034.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15960612