Accession Number:

AD0092213

Title:

WIND-TUNNEL INVESTIGATION OF A RAM-JET MISSILE MODEL HAVING A WING AND CANARD SURFACES OF DELTA PLAN FORM WITH 70 SWEPT LEADING EDGES. FORCE AND MOMENT CHARACTERISTICS AT COMBINED ANGLES OF PITCH AND SIDESLIP FOR MACH NUMBER 2.01

Descriptive Note:

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA

Personal Author(s):

• Driver, Cornelius
• Hamilton, Clyde V.

Report Date:

1956-04-26

Pagination or Media Count:

70.0

Abstract:

Descriptors:

• *GUIDED MISSILES
• *SWEPT WINGS
• *SUPERSONIC FLOW
• *RAMJET TEST VEHICLES
• *CANARD CONFIGURATIONS
• CONTROL SYSTEMS
• WIND TUNNEL TESTS
• SIDESLIP
• MODEL TESTS
• PITCH(INCLINATION)

Subject Categories:

• Guided Missile Dynamics, Configurations and Control Surfaces

Distribution Statement:

APPROVED FOR PUBLIC RELEASE