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![The Impact of Organizational Culture on KC-135 Combat Education and Training]( "The Impact of Organizational Culture on KC-135 Combat Education and Training")
The Impact of Organizational Culture on KC-135 Combat Education and Training59,99 €![A Comparative Study Of KC-135 Operations in Vietnam, Desert Storm, and Allied Force]( "A Comparative Study Of KC-135 Operations in Vietnam, Desert Storm, and Allied Force")
A Comparative Study Of KC-135 Operations in Vietnam, Desert Storm, and Allied Force59,99 €![Improving Wartime Spares Support to AMC: An Analysis of Kc-135 Readiness Spares Packages During Operation Allied Force with a Look to the Future and S]( "Improving Wartime Spares Support to AMC: An Analysis of Kc-135 Readiness Spares Packages During Operation Allied Force with a Look to the Future and S")
Improving Wartime Spares Support to AMC: An Analysis of Kc-135 Readiness Spares Packages During Operation Allied Force with a Look to the Future and S59,99 €![KC-135 Recapitalization Issues]( "KC-135 Recapitalization Issues")
KC-135 Recapitalization Issues59,99 €![Reballasting the KC-135 Fleet for Fuel Efficiency]( "Reballasting the KC-135 Fleet for Fuel Efficiency")
Reballasting the KC-135 Fleet for Fuel Efficiency59,99 €![Tanker Force Structure: Recapitalization of the Kc-135]( "Tanker Force Structure: Recapitalization of the Kc-135")
Tanker Force Structure: Recapitalization of the Kc-13559,99 €![Forecasting the Kc-135 Cost Per Flying Hour: A Panel Data Analysis]( "Forecasting the Kc-135 Cost Per Flying Hour: A Panel Data Analysis")
Forecasting the Kc-135 Cost Per Flying Hour: A Panel Data Analysis60,99 €
This research effort examines the static affects of a KC-135 flowfield on a flexible winged Sensorcraft model. The KC-135 flowfield data is generated by a vortex lattice code and integrated into Sensorcraft model for analysis. Building on previous research, a refueling situation was modeled to note the effects of the Sensorcraft at varying locations within the flowfield. The Sensorcraft model was analyzed for both rigid and flexible wings as a means of comparision. Flowfield locations of interest were determined and trimmed conditions were computed for each flowfield location.