Reply to Technical Comment from R. O. Hessler and R. L. Glick von Dotson, K. W

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Vortex Shedding in a Large Solid Rocket Motor Without Inhibitors at the Segment Interfaces von Dotson, K W, Koshigoe, S, Pace, K K

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Vortex-induced vibration of a heavy-lift launch vehicle during transonic flight von Dotson, K.W, Engblom, W.A

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Limit-Cycle Oscillation Induced by Nonlinear Aerodynamic Forces von Dotson, K. W, Baker, R. L, Sako, B. H

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Transient Coupling of Launch Vehicle Bending Responses with Aerodynamic Flow State Variations von Dotson, K. W

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Structural Dynamic Analysis of Solid Rocket Motor Resonant Burning von Dotson, K. W, Womack, J. M, Grosserode, P. J

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LAUNCH VEHICLE BUFFETING WITH AEROELASTIC COUPLING EFFECTS von DOTSON, K.W., BAKER, R.L., SAKO, B.H.

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Launch Vehicle Dynamic and Control Effects from Solid Rocket Motor Slag Ejection von Dotson, K. W, Murdock, J. W, Kamimoto, D. K

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Launch Vehicle Self-Sustained Oscillation from Aeroelastic Coupling Part 1: Theory von Dotson, K. W, Baker, R. L, Sako, B. H

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Launch Vehicle Self-Sustained Oscillation from Aeroelastic Coupling Part 2: Analysis von Dotson, K. W, Baker, R. L, Bywater, R. J

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Formulation and analysis of launch vehicle maneuvering loads von Dotson, K. W, Tiwari, S. B

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Vortex Shedding in a Large Solid Rocket Motor Without Inhibitors at the Segment Interfaces von Dotson, K. W, Koshigoe, S, Pace, K. K

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Dynamic Response of Simple Systems to Periodic Forces von Veletsos, A. S, Dotson, K. W, Ventura, C. E

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Vertical and torsional impedances for radially inhomogeneous viscoelastic soil layers von Dotson, K.W., Veletsos, A.S.

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Vertical and Torsional Vibration of Foundations in Inhomogeneous Media von Veletsos, Anestis S, Dotson, Kirk W

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Mission-Specific Pogo Stability Analysis with Correlated Pump Parameters von Dotson, Kirk W, Rubin, Sheldon, Sako, Brian H

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Impedances of Soil Layer with Disturbed Boundary Zone von Veletsos, Anestis S, Dotson, Kirk W

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Limit-cycle oscillation induced by nonlinear aerodynamic forces von Dotson, K. W., Baker, R. L., Sako, B. H.

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Launch vehicle self-sustained oscillation from aeroelastic coupling. II - Analysis von Dotson, K W, Baker, R L, Bywater, R J

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Launch vehicle self-sustained oscillation from aeroelastic coupling. I - Theory von Dotson, K W, Baker, R L, Sako, B H

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