Accession Number:

AD0092432

Title:

INVESTIGATION BY THE TRANSONIC-BUMP METHOD OF A 35 deg SWEPTBACK SEMISPAN MODEL EQUIPPED WITH A FLAP OPERATED BY A SERIES OF SERVOVANES LOCATED AHEAD OF AND GEARED TO THE FLAP

Descriptive Note:

Technical note

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA

Personal Author(s):

• Phillips, William H.
• Thompson, Robert F.

Report Date:

1956-04-01

Pagination or Media Count:

44.0

Abstract:

Descriptors:

• *AERODYNAMIC CHARACTERISTICS
• *CONTROL SURFACES
• AIRFOILS
• DRAG
• LIFT
• SERVOMECHANISMS

Subject Categories:

• Aircraft
• Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE