Accession Number:

ADB805337

Title:

Considerations of the Total Drag of Supersonic Airfoil Sections

Descriptive Note:

Technical note

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA

Personal Author(s):

Report Date:

1947-07-01

Pagination or Media Count:

26.0

Abstract:

Descriptors:

Subject Categories:

  • Aerodynamics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE