Analysis of the Flow Past a Shockless Lifting Airfoil in Design and Off-Design Conditions.
Abstract
A shockless lifting airfoil designed for shockless inviscid flow at transonic vleocity was tested at high Reynolds numbers in design and off-design conditions. The experimental results are compared against theoretical results, showing in general good agreement.
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 01, 1971
- Accession Number
- AD0734760
Entities
People
- D. G. Korn
- J. J. Kacprznski
- L. H. Ohman
- P. R. Garabedian
Organizations
- National Research Council Canada