Accession Number:

AD0092214

Title:

INVESTIGATION AT HIGH SUBSONIC SPEEDS OF SOME EFFECTS OF SIDESLIP ON THE AERODYNAMIC LOADS ON FINNED AND UNFINNED BODIES MOUNTED FROM THE SWEPT-WING OF A WING-FUSELAGE MODEL

Descriptive Note:

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA

Personal Author(s):

• King, Jr, Thomas J.

Report Date:

1956-04-26

Pagination or Media Count:

56.0

Abstract:

Descriptors:

• *LOAD DISTRIBUTION
• *WING BODY CONFIGURATIONS
• *AIRCRAFT PROTUBERANCES
• *FINS
• SWEPT WINGS
• AERODYNAMIC LOADING
• SUBSONIC FLOW
• OGIVES

Subject Categories:

• Aerodynamics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE