It is demonstrated that the temperature profiles of jets expanding into a supersonic stream are considerably smaller than the temperature profiles of jets expanding into quiescent air. The effect on the wake of varying afterbody geometry is shown to be small. The gross spreading characteristics of jets expanding from convergent and convergent-divergent nozzles in the base of a body of revolution with various boattail configurations at a Mach number of 1.91 are presented
Detailed knowledge of jet plume development in the near-field (the first 10–15 nozzle exit diameters...
An investigation was conducted of isolated convergent-divergent nozzles to determine the effect of s...
A study of a flow through a straight converging-diverging nozzle of simple design has been made prel...
It is demonstrated that the temperature profiles of jets expanding into a supersonic stream are cons...
The Mach number and temperature profiles in jets expanding from convergent and convergent-divergent ...
A series of rocket motors with varying exit to throat area ratios was tested in the 8- by 6-foot win...
An investigation of the jet-spreading characteristics of a 16 inch ram-jet engine was conducted in t...
The interaction of the flow from one convergent and two convergent-divergent nozzles on parabolic af...
An investigation was conducted in the 8-by-6 foot supersonic wind tunnel on the effect of exhaust-ga...
The spreading characteristics of jets from several asymmetric nozzles are studied in comparison to t...
Preliminary results are presented from an investigation to determine the influence of afterbody geom...
An experimental investigation of a series of four convergent-divergent exhaust nozzles was conducted...
A wind-tunnel investigation to determine the effects of both single and twin jets on base drag of a ...
A parametric investigation has been conducted to determine the jet effects on the boattail drag of n...
An investigation was made at free-stream Mach numbers of 1.62, 1.93, and 2.41 to determine the effec...
Detailed knowledge of jet plume development in the near-field (the first 10–15 nozzle exit diameters...
An investigation was conducted of isolated convergent-divergent nozzles to determine the effect of s...
A study of a flow through a straight converging-diverging nozzle of simple design has been made prel...
It is demonstrated that the temperature profiles of jets expanding into a supersonic stream are cons...
The Mach number and temperature profiles in jets expanding from convergent and convergent-divergent ...
A series of rocket motors with varying exit to throat area ratios was tested in the 8- by 6-foot win...
An investigation of the jet-spreading characteristics of a 16 inch ram-jet engine was conducted in t...
The interaction of the flow from one convergent and two convergent-divergent nozzles on parabolic af...
An investigation was conducted in the 8-by-6 foot supersonic wind tunnel on the effect of exhaust-ga...
The spreading characteristics of jets from several asymmetric nozzles are studied in comparison to t...
Preliminary results are presented from an investigation to determine the influence of afterbody geom...
An experimental investigation of a series of four convergent-divergent exhaust nozzles was conducted...
A wind-tunnel investigation to determine the effects of both single and twin jets on base drag of a ...
A parametric investigation has been conducted to determine the jet effects on the boattail drag of n...
An investigation was made at free-stream Mach numbers of 1.62, 1.93, and 2.41 to determine the effec...
Detailed knowledge of jet plume development in the near-field (the first 10–15 nozzle exit diameters...
An investigation was conducted of isolated convergent-divergent nozzles to determine the effect of s...
A study of a flow through a straight converging-diverging nozzle of simple design has been made prel...
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