Eric Wintenberger, Ph.D.

Affiliations: 
2004 California Institute of Technology, Pasadena, CA 
Area:
Aerospace Engineering, Mechanical Engineering
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"Eric Wintenberger"

Parents

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Joseph E. Shepherd grad student 2004 Caltech
 (Application of steady and unsteady detonation waves to propulsion.)
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Publications

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Wintenberger E, Shepherd JE. (2006) Introduction to "to the question of energy use of detonation combustion" by Ya. B. Zel'dovich Journal of Propulsion and Power. 22: 586-587
Wintenberger E, Shepherd JE. (2006) Model for the performance of airbreathing pulse-detonation engines Journal of Propulsion and Power. 22: 593-603
Wintenberger E, Shepherd JE. (2006) Stagnation Hugoniot analysis for steady combustion waves in propulsion systems Journal of Propulsion and Power. 22: 835-844
Wintenberger E, Shepherd JE. (2006) Thermodynamic cycle analysis for propagating detonations Journal of Propulsion and Power. 22: 694-697
Wintenberger E, Austin JM, Cooper M, et al. (2004) Reply to Comment on "Analytical Model for the Impulse of Single-Cycle Pulse Detonation Tube" by W.H. Heiser and D.T. Pratt Journal of Propulsion and Power. 20: 189-191
Wintenberger E, Austin JM, Cooper M, et al. (2004) Erratum for "Analytical Model for the Impulse of Single-Cycle Pulse Detonation Tube" Journal of Propulsion and Power. 20: 765-767
Wintenberger E, Cooper M, Pintgen F, et al. (2004) Reply to Comment on "Analytical Model for the Impulse of Single Cycle Pulse Detonation Tube" by M. I. Radulescu and R. K. Hanson Journal of Propulsion and Power. 20: 957-959
Radulescu MI, Hanson RK, Wintenberger E, et al. (2004) Comment on "analytical model for the impulse of single-cycle pulse detonation tube", Journal of Propulsion and Power. 20: 956-959
Heiser WH, Pratt DT, Wintenberger E, et al. (2004) Comment on "Analytical Model for the Impulse of Single-Cycle Pulse Detonation Tube" by E. Wintenberger, et al. (multiple letters) Journal of Propulsion and Power. 20: 189-191
Wintenberger E, Shepherd JE. (2004) Thermodynamic analysis of combustion processes for propulsion systems Aiaa Paper. 12568-12585
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