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The leading-edge effects on the laminar flat- plate boundary layer and the aerodynamic heating at Mach 10.4.

Author
Stone, H. W.
Published
May 1, 1969.
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
Leading edge effects on laminar flat plate boundary layer and aerodynamic heating at Mach 10.4
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19690014093.
Accession ID: 69N23467.
NASA-TN-D-5160.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15953688