Analytical Modeling of Supersonic Retropropulsion Plume Structures
Cordell, C.E.; and Braun, R.D.; "Analytical Modeling of Supersonic Retropropulsion Plume Structures," Journal of Spacecraft and Rockets, Vol. 50, No. 4, pp. 763-770, July-Aug, 2013.
Multi-Fidelity Approach to Estimate Heating for Three-Dimensional Hypersonic Aeroshells
Bopp, M.S.;Ruffin, S.M.;Braun, R.D.;Clark, I.G.; and Theisinger, J.T.; "Multi-Fidelity Approach to Estimate Heating for Three-Dimensional Hypersonic Aeroshells," Journal of Spacecraft and Rockets, Vol. 50, No. 4, pp. 754-762, July-Aug, 2013.
hree-Dimensional Finite Element Ablative Thermal Response and Design of Thermal Protection Systems
Dec, J.A.; and Braun, R.D.; "Three-Dimensional Finite Element Ablative Thermal Response and Design of Thermal Protection Systems," Journal of Spacecraft and Rockets, Vol. 50, No. 4, pp. 725-734, July-Aug, 2013.
Space-Based Distributed Computing Using a Networked Constellation of Small Satellites
Gunter, B.C.; and Maessen, D.C.; "Space-Based Distributed Computing Using a Networked Constellation of Small Satellites", Journal of Spacecraft and Rockets, Vol. 50, No. 5, pp. 1086-1095, Sept-Oct, 2013.
Guided Entry Performance of Low Ballistic Coefficient Vehicles at Mars
Meginnis, I.M.;Putnam, Z.R.;Clark, I.G.;Braun, R.D.; and Barton, G.H.; "Guided Entry Performance of Low Ballistic Coefficient Vehicles at Mars," Journal of Spacecraft and Rockets, Vol. 50, No. 5, pp. 1047-1059, Sept-Oct, 2013.
Application of a Reynolds-Averaged Navier-Stokes Approach to Supersonic Retropropulsion Flowfields
Korzun, A.M.; and Braun, R.D.; "Application of a Reynolds-Averaged Navier-Stokes Approach to Supersonic Retropropulsion Flowfields," Journal of Spacecraft and Rockets, Vol. 50, No. 5, pp. 961-980, Sept-Oct, 2013.