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


Corporate Author : NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA


Personal Author(s) : Driver, Cornelius ; Hamilton, Clyde V


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/092213.pdf


Report Date : 26 Apr 1956


Pagination or Media Count : 70


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 Dynam, Config & Cntrl Surfaces


Distribution Statement : APPROVED FOR PUBLIC RELEASE