djkingsley
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- Feb 22, 2014
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My next project is to venture into HPR clustering and airstarts. One might ask why and the only answer I have is "cause I want to". BourbonRoc is a upscale Bourbon bottle with a cental 98mm and four 75mm motor mounts. Flight stability is controlled by the addition of four 5 gallon Bourbon barrels vaguely resembling tube fins.
BourbonRoc is the epitome of low and slow, the whole flight profile is designed around 1000-1500 ft apogee taking inspiration from TomC's projects.
I have modeled the project in Rhino for the geometry, spreadsheets for the weights and centers, CFD for the center of pressure, and OpenRocket for altitude/stability predictions.
Weights & Centers: View attachment BourbonRocWeightEstimate.pdf
Introducing BourbonRoc:
CFD was used to predict the center of pressure for a range of velocities, the following image shows the pressure on the rocket and streamlines in the flow for 3 degrees Angle of Attack (AoA).
The next image shows a vertical section through the computational domain with velocity contours. The large area of recirculating flow aft of the rocket gives indication of the magnitude of the base drag component BourbonRoc will be subject to.
Center of Pressure: View attachment BourbonRocCFD.pdf
I am targeting MDRA's spring Red Glare 2018 for this project, the sonotube has been ordered and discussions with Python Rocketry are underway for the nosecone and transition pieces.
Since the main objective is HPR clustering and airstarts, I have ordered/received a LOC Warlock customized with a central 54mm and four 29mm motor mounts to gain the experience needed to safely fly BourbonRoc. Due to its size and complexity BourbonRoc will be flown on its central 98mm motor for one or more shake down flights prior to flying on its full cluster.
This thread will serve as a central build thread for both BourbonRoc and the Warlock, including discussions on best practices on HPR clustering and airstarts as it pertains to these two rockets.
Coming up next will be CAD drawings for the custom nose cone and transition pieces.
BourbonRoc is the epitome of low and slow, the whole flight profile is designed around 1000-1500 ft apogee taking inspiration from TomC's projects.
I have modeled the project in Rhino for the geometry, spreadsheets for the weights and centers, CFD for the center of pressure, and OpenRocket for altitude/stability predictions.
Weights & Centers: View attachment BourbonRocWeightEstimate.pdf
Introducing BourbonRoc:
CFD was used to predict the center of pressure for a range of velocities, the following image shows the pressure on the rocket and streamlines in the flow for 3 degrees Angle of Attack (AoA).
The next image shows a vertical section through the computational domain with velocity contours. The large area of recirculating flow aft of the rocket gives indication of the magnitude of the base drag component BourbonRoc will be subject to.
Center of Pressure: View attachment BourbonRocCFD.pdf
I am targeting MDRA's spring Red Glare 2018 for this project, the sonotube has been ordered and discussions with Python Rocketry are underway for the nosecone and transition pieces.
Since the main objective is HPR clustering and airstarts, I have ordered/received a LOC Warlock customized with a central 54mm and four 29mm motor mounts to gain the experience needed to safely fly BourbonRoc. Due to its size and complexity BourbonRoc will be flown on its central 98mm motor for one or more shake down flights prior to flying on its full cluster.
This thread will serve as a central build thread for both BourbonRoc and the Warlock, including discussions on best practices on HPR clustering and airstarts as it pertains to these two rockets.
Coming up next will be CAD drawings for the custom nose cone and transition pieces.