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

Report Date:

1956-04-26

Pagination or Media Count:

70.0

Abstract:

Subject Categories:

  • Guided Missile Dynamics, Configurations and Control Surfaces

Distribution Statement:

APPROVED FOR PUBLIC RELEASE