Accession Number:

AD0092212

Title:

FREE-FLIGHT INVESTIGATION OF THE CONTROL EFFECTIVENESS OF A DIFFERENTIALLY DEFLECTED HORIZONTAL TAIL AT MACH NUMBERS FROM 0.8 TO 1.6

Descriptive Note:

Research memo.

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA

Personal Author(s):

• Mitchell, Jesse L.
• Vitale, A. James

Report Date:

1956-04-26

Pagination or Media Count:

28.0

Abstract:

Descriptors:

• *ROLL
• *HORIZONTAL STABILIZERS
• *ROCKET MODELS
• TAIL ASSEMBLIES
• TRANSONIC CHARACTERISTICS
• REMOTELY PILOTED VEHICLES

Subject Categories:

• Aerodynamics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE