科技报告详细信息
Formulation and Implementation of Inflow/Outflow Boundary Conditions to Simulate Propulsive Effects
Rodriguez, David L ; Aftosmis, Michael ; Nemec, Marian
关键词: AIRCRAFT DESIGN;    BOUNDARY CONDITIONS;    COMPUTATIONAL FLUID DYNAMICS;    COMPUTERIZED SIMULATION;    FLOW VELOCITY;    HYPERSONICS;    INFORMATION FLOW;    MASS FLOW RATE;    PROPULSION SYSTEM CONFIGURATIONS;    PROPULSION SYSTEM PERFORMANCE;    SHAPE OPTIMIZATION;    SYSTEMS ENGINEERING;    AERODYNAMIC CHARACTERISTICS;    AERODYNAMIC CONFIGURATIONS;    GRID GENERATION (MATHEMATICS);    RUNGE-KUTTA METHOD;    SUBSONIC FLOW;   
RP-ID  :  ARC-E-DAA-TN51324
美国|英语
来源: NASA Technical Reports Server
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