Pages that link to "Item:Q1403655"

The following pages link to Effect of gas non-ideality on the performance of Laval nozzles with an abrupt constriction (Q1403655):

Displaying 16 items.

• Inviscid gas flows in nozzles with a steeply converging contour (Q431754) (← links)
• Contouring the nozzles producing a uniform supersonic flow or a thrust maximum in the presence of a curvilinear sonic line (Q431755) (← links)
• Optimal supersonic nozzles with power-law generators (Q538942) (← links)
• Hysteresis phenomena in a plane rotatable nozzle (Q545828) (← links)
• Real gas effects in thermally choked nozzle flows (Q1328421) (← links)
• Loss of specific impulse due to friction in spike nozzles (Q1402823) (← links)
• Calculating the thrust characteristics of nozzles from their outlet cross-section parameters (Q1403705) (← links)
• Analysis of the thrust characteristics of jet nozzles designed by various methods (Q1580157) (← links)
• The influence of heat supply on the gas dynamical parameters of gas flow in a Laval nozzle (Q1803118) (← links)
• Choking of ideal-gas flow in convergent nozzles and integral nozzle characteristics (Q1815184) (← links)
• Stability of one-dimensional steady flows with detonation wave in a channel of variable cross-sectional area (Q2207548) (← links)
• Comparison of air-breathing engines with slow and detonation combustion (Q2238181) (← links)
• Study of the aerodynamic characteristics of chevron nozzles on the basis of a numerical calculation of the flowfield (Q2387897) (← links)
• Convergent-divergent nozzle under highly overexpanded conditions (Q2388172) (← links)
• (Q5186954) (← links)
• NIMOC: a design and analysis tool for supersonic nozzles under non-ideal compressible flow conditions (Q6136538) (← links)