Accession Number:

ADB806009

Title:

Wind-Tunnel Investigation of Effect of Yaw on Lateral-Stability Characteristics. 3 - Symmetrically Tapered Wing at Various Positions on Circular Fuselage with and without a Vertical Tail

Descriptive Note:

Technical note

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA

Personal Author(s):

• Recant, Isidore G.
• Wallace, Arthur R.

Report Date:

1941-09-01

Pagination or Media Count:

28.0

Abstract:

Descriptors:

• *AERODYNAMIC STABILITY
• TAILS(AIRCRAFT)
• FUSELAGES
• TAPER
• TAIL ASSEMBLIES
• AIRFOILS

Subject Categories:

• Aerodynamics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE