Accession Number:

AD0029198

Title:

FLIGHT INVESTIGATION OF THE EFFECTS OF A PARTIAL-SPAN LEADING-EDGE CHORD EXTENSION ON THE AERODYNAMIC CHARACTERISTICS OF A 35 deg SWEPT-WING FIGHTER AIRPLANE

Descriptive Note:

Research memo.

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMINISTRATION MOFFETT FIELD CA AMES RESEARCH CENTER

Report Date:

1954-04-23

Pagination or Media Count:

39.0

Abstract:

Subject Categories:

  • Aircraft
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE