Actions for Langley hotshot tunnel operations with helium at Mach numbers in excess of 30.

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Langley hotshot tunnel operations with helium at Mach numbers in excess of 30.

Author
Miller, C. G., III
Published
Jul 1, 1970.
Physical Description
1 electronic document
Online Version

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Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
Temperature and pressure effects on high Mach number helium flow in hotshot wind tunnel
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19700024440.
Accession ID: 70N33751.
NASA-TN-D-5901.
L-6876.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15951271