Шийко, Александр Николаевич
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No 3 (2017): Aerospace technic and technology - Aerodynamics, dynamics, ballistics and flight control of aircraft
RESULTS OF THE RESEARCH OF STATIC PRESSURE DISTRIBUTION ON THE HEAD PART MISSILE M-100 AERO PHYSICAL SYSTEMS ON THE BASIS OF THE NUMERICAL METHOD OF CALCULATION AND FLIGHT EXPERIMENT FOR MACH NUMBERS 1,4 М4,2, REYNOLDS ReL, ≤108 , ACCELERATION a ≤32g IN THE CONDITIONS OF AERODYNAMIC HEATING
Abstract PDF (Русский)
ISSN: 2663-2217