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Development of a 3D Grain Burnback Simulation Tool for Solid Rocket Motors

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Advances in Sustainable Aviation

Abstract

The study presents the newly developed fast three-dimensional grain burnback tool. The computational method that has been developed is based on minimum distance calculation technique. Structured grid for computational domain modeling has been used, and grid based-surface propagation method has been utilized for grain burnback simulation by using STL and SLP file formats. The developed simulation tool is able to solve very complex grain geometries. The auto mesh interface tool has been tested for quite complex grain geometries. The solution domain has been created properly without any user interference. It is observed that the determined specific distance ratio gives an acceptable accuracy within a short computation time. The burnback simulations of a real solid rocket motor indicate that the symmetrical model used with the initial distance calculation method provides an important computational time improvements. The burnback analysis of symmetrical models, initial distance calculation method, and distance calculation without sign correction methods are the originalities of the current tool. In addition, the use of SLP file format in burnback simulation and the mesh interface implementation of the developed tool significantly reduces the required total amount of user interaction for the initialization of the burnback model. This also reduces total simulation time and the error due to the user interaction.

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Abbreviations

∀:

Volume

A b :

Burning surface area

C:

Corner

CAD:

Computer-aided design

d :

Distance value

d b :

Burning distance

dx, dy, dz :

Structured grid dimension

MDF:

Minimum distance function

MDV:

Minimum distance value

n :

Number of points in any axis

N:

Number of slices

P:

Intersection point

Per :

Perimeter

SLP:

Rendering file format

STL:

Standard Template Library

V′:

Extruded vertex

w inc :

Web increment

w max :

Maximum web thickness

x, y, z :

Cartesian space coordinates

α :

Angle between two vectors

References

  1. Coats, D.E., Nickerson, G.R., Dang, A.L., Dunn, S.S., Kehtarnavaz, H. (1987). Solid Performance Program (SPP). In Proceeding of 23rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference San Diego, CA, U.S.A. June 29–July 2 1987, AIAA 1987-1701.

    Google Scholar 

  2. Dunn, S.S., & Coats, D.E. (1997). 3-D grain design and ballistic analysis using the SPP97 code. In Proceeding of 33rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Seattle, WA, U.S.A., 1997, AIAA 97-3340.

    Google Scholar 

  3. Zeller, B. (2005). Solid propellant grain design. In A. Davenas (Ed.), Solid rocket propulsion technology (1st English ed., pp. 35–84). New York: Pergamon Press.

    Google Scholar 

  4. Toker, K.A., Tınaztepe, H.T., Aksel, M.H., (2004). Three-dimensional propellant grain burnback calculations on tetrahedron mesh by fast marching method. In Proceeding of 22nd Applied Aerodynamics Conference and Exhibit, Rhode Island, 16–19 August 2004, AIAA-2004-4960.

    Google Scholar 

  5. Peterson, E.G., Nielson, G.C., Johnson, W.C., Cook, K.S., Barron, J.G. (1968). Generalized coordinate grain design and internal ballistics evaluation program. In Proceeding of CPIA/AIAA 3rd Solid Propulsion Conference June 1968.

    Google Scholar 

  6. Willcox, M.A., Brewster, M.Q., Tang, K.C., Stewart, D.S. (2005). Solid propellant grain design and burnback simulation using a minimum distance function. In Proceeding of 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Tucson, Arizona, 10–13 July 2005, AIAA 2005-4350.

    Google Scholar 

  7. Malosio, M., Pedrocchi, N., Tosatti, L. M. (2009). Algorithm to offset and smooth tessellated surfaces. In Computer-aided design and applications (pp. 351–363).

    Google Scholar 

  8. Qu, X., & Stucker, B. (2003). A 3D surface offset method for STL-format models. Rapid Prototyping Journal, 9(3), 133–141.

    Article  Google Scholar 

  9. Stucker, B., & Qu, X. (2003). A finish machining strategy for rapid manufactured parts and tools. Rapid Prototyping Journal, 9(4), 194–200.

    Article  Google Scholar 

  10. Hartfield, R., Jenkins, R., Burkhalter, J., Foster, W. (2003). A review of analytical methods for solid rocket motor grain analysis. In Proceeding of 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Huntsville, Alabama, July 2003, AIAA 2003-4506.

    Google Scholar 

  11. Pavić, D., & Kobbelt, L. (2008). High-resolution volumetric computation of offset surfaces with feature preservation. Computer Graphics Forum, 27(2), 165–174.

    Article  Google Scholar 

  12. Koç, B., & Lee, Y. S. (2002). Non-uniform offsetting and hollowing objects by using biarcs fitting for rapid prototyping processes. Computers in Industry, 47, 1–23. 2002.

    Article  Google Scholar 

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Correspondence to D. Funda Kurtulus .

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Ata, Y., Kurtulus, D.F., Arkun, O.U. (2018). Development of a 3D Grain Burnback Simulation Tool for Solid Rocket Motors. In: Karakoç, T., Colpan, C., Şöhret, Y. (eds) Advances in Sustainable Aviation. Springer, Cham. https://doi.org/10.1007/978-3-319-67134-5_5

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  • DOI: https://doi.org/10.1007/978-3-319-67134-5_5

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  • Online ISBN: 978-3-319-67134-5

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