Aeronautics & Astronautics - Fluid Sciences > Aerodynamics: Page 7

No. 30071 Reflection of shock waves: reflected shock No. 30072 Traveling wave in tube: propagation over time No. 30073 Time-space frame for shock wave reflection analysis No. 30074 Wave propagation: configuration No. 30075 Wave propagation: density distribution at time 1 No. 30076 Wave propagation: density distribution at time 2 No. 30077 Wave propagation: aging of wave structure phase 1 No. 30078 Wave propagation: aging of wave structure phase 2 No. 30079 Wave propagation: aging of wave structure phase 3 No. 30080 Sound waves in opposite direction along with their shocks No. 30081 Density distribution of finite nonlinear wave No. 30082 Temperature distribution of finite nonlinear wave No. 30083 Speed of sound distribution of finite nonlinear wave No. 30084 Flow velocity distribution of finite nonlinear wave No. 30085 Wave shape distortion: time 1 No. 30086 Wave shape distortion: time 2 No. 30087 Wave shape distortion: time 3 No. 30088 Wave shape distortion: time 4 No. 30089 Time space frame for flow path analysis No. 30090 Method of characteristics: using 2 paths to reduce analysis complexity No. 30091 Expansion wave: two pressures separated by diaphragm No. 30092 Expansion wave: wave's head and tail and its propagation No. 30093 Time-space frame for expansion wave analysis No. 30094 Expansion region in expansion wave No. 30095 Wave propagation in expansion wave phenomena No. 30096 Wave velocity spatial plot in expansion wave phenomena No. 30097 Density spatial distribution in expansion wave phenomena No. 30098 Temperature spatial distribution in expansion wave phenomena No. 30099 Pressure spatial distribution in expansion wave phenomena No. 30100 Shock tube: two pressures separated by diaphragm No. 30101 Shock tube: shock wave and expansion wave propagation No. 30102 Space-time frame for shock tube analysis No. 30103 Fluid velocity in shock tube phenomena No. 30104 Fluid pressure in shock tube phenomena No. 30105 Temperature of fluid in shock tube phenomena No. 30106 Conical flow: plane defined by constant potential No. 30107 Conical flow with perspective view No. 30108 Conical flow along body or revolution: use of cylindrical coordinate No. 30109 Shock wave in conical flow along body of revolution No. 30110 Illustration of numerical procedures to analyze shock over cone No. 30111 Relationship between mach numbers and cone angles No. 30112 Cone and shock angle diagram: comparison of wedge and cone bodies No. 30113 Maximum cone angle vs. mach number at various adiabatic indexes No. 30114 Surface pressure coefficients vs. cone angles at various Mach numbers No. 30115 Surface pressure coefficients vs. cone angles at various Mach numbers No. 30116 Thin shock layer on wedge body at Mach number of 2 No. 30117 Thin shock layer on wedge body at Mach number of 20 No. 30118 Entropy layer on blunt-nosed body No. 30119 Temperature profile of flow due to viscous interaction No. 30120 Pressure distribution along conical body influenced by viscous effect
 

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