Aerodynamic characteristics at Mach numbers from 1.60 to 2.16 of a blunt-nose missile model having a triangular cross section and fixed triform fins

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Summary:

Aerodynamic characteristics at Mach numbers 1.60 to 2.16 of blunt-nose missile model having triangular cross section and fixed triform fins

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Collection:

NASA Technical Reports Server (NTRS) Collection.

Note:

Document ID: 19710022735.
Accession ID: 71N32211.
NASA-TM-X-2340.
L-7179.

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View MARC record | catkey: 15948802