Measurement of Pressure on an Oscillating Aileron in Transonic Flow,
Abstract
The report gives the results of pressure measurements on an oscillating aileron in plane-parallel transonic flow. The measurements were made using pressure sensors inside the model in a regime of forced oscillations at M = 0.974.
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 29, 1973
- Accession Number
- AD0769982
Entities
People
- T. P. Nevezhina
- V. V. Mazarenko
Organizations
- National Air and Space Intelligence Center