Accession Number:

AD0256080

Title:

TRANSONIC INVESTIGATION OF AERODYNAMIC CHARACTERISTICS OF A SWEPT-WING FIGHTER-AIRPLANE MODEL WITH LEADING-EDGE DROOP IN COMBINATION WITH OUTBOARD CHORD-EXTENSIONS AND NOTCHES

Descriptive Note:

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON D C

Report Date:

1961-05-01

Pagination or Media Count:

1.0

Abstract:

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE