Accession Number:

AD0255195

Title:

INVESTIGATION AT HIGH SUBSONIC SPEEDS OF THE USE OF LOW AUXILIARY TAIL SURFACES HAVING DIHEDRAL TO IMPROVE THE LONGITUDINAL AND DIRECTIONAL STABILITY OF A T-TAIL MODEL AT HIGH LIFT

Descriptive Note:

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON D C

Personal Author(s):

• SLEEMAN,WILLIAM C. JR.

Report Date:

1961-04-01

Pagination or Media Count:

1.0

Abstract:

Descriptors:

• *HORIZONTAL STABILIZERS
• *SUBSONIC FLOW
• AIRFOILS
• ASPECT RATIO
• LIFT
• ROLL
• STABILITY
• TAILS(AIRCRAFT)

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE