- Restrictions on Access:
- Unclassified, Unlimited, Publicly available.
- The use of a pitot-static probe to determine wing section drag at speeds from Mach 0.5 to approximately 1.0 was evaluated in flight. The probe unit is described and operational problems are discussed. Typical wake profiles and wing section drag coefficients are presented. The data indicate that the pitot-static probe gave reliable results up to speeds of approximately 1.0.
- NASA Technical Reports Server (NTRS) Collection.
- Document ID: 19740021257.
Accession ID: 74N29370.
- No Copyright.
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