Accession Number:

AD0734760

Title:

Analysis of the Flow Past a Shockless Lifting Airfoil in Design and Off-Design Conditions.

Descriptive Note:

Aeronautical rept.,

Corporate Author:

NATIONAL AERONAUTICAL ESTABLISHMENT OTTAWA (ONTARIO)

Report Date:

1971-11-01

Pagination or Media Count:

83.0

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.

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE