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i, 2_ 3. . , . , 1 , i0. ii. 12. 13. REFERENCES Sabiers, R.L., Stek, J.B., Boost Pumps Design Criteria Monograph, Contract NAS 3-11176, AGC 9400-8 (Conf.), February 1968 Jekat, W.Ao, The Worthington Inducer, NAS 8-2680, February 1964 Farquhar, J., Lindley, BoK., McKinney, E.B., Olson, G.K., Buckman, P.S., Inducer Dynamics Full-Flow, Full-Admission Hydraulic Turbine Drive, NASA CR-72566, August 1969 Farquhar, J. and Lindley, B.K., Hydraulic Design of the M-I Liquid Hydrogen TurbopumD, NASA CR-54822, 15 July 1966 Farquhar, J., Viteri, P., Axial Flow Pumpsj Design Criteria Monograph, Contract NAS 3-10293, AGC 9400-6 Rev. i, July 1968 Taylor, W.E., Murrin, T.A., Colombo, R.M., Systematic Two-Dimensional Cascade Testing Vol. 1 - Double Circular-Arc Hydrofoils, NASA CR-72498, December 1969 Cunnan, W.S., Kovich, G., Reemsnyder, D.C., Effect of Fluid Temperature on the Cavitation Performance of a High Hub-Tip Ratio Axial Flow Pump in Water to 250°F (394 K), NASA TN D-5318, July 1969 Crouse, J.E., Soltis, R.F., and Montgomery, J.C., Investigation of the Performance of an Axial Flow-Pump Stage Designed by the Blade Element Theory, NASA TN D-If09, December 1966 Crouse, J.E. and Sandercock, D.M., Design and Over-all Performance of an Axial-Flow Pump Rotor with a Blade Tip Diffusion Factor of 0.43, NASA TN D-2295, May 1964 Miller, M.J. and Crouse, J.E., Design and Over-all Performance of an Axial-Plow Pump Rotor with a Blade Tip D_ffusion Factor of 0.66, NASA TN D-3024, September 1965 Crouse, J.E., and Sandercock, D.M., Blade Element Performance of Two- Stage Axial-Flow Pump with Tandem-Row Inlet Stage, NASA TN-3962, May 1967 Stripling, L.B., "Cavitation in Turbopumps - Part 2," Trans. ASME, Journal of Basic Engineering, Vol. 84, 1962, pp. 339-350 Jakobsen, J.K., Design Cr$teria Monograph Pump Inducers, Rocketdyne Report R-7422, NAS 3-11180, March 1968 127PDF Image | HUBLESS INDUCER FLOW HYDRAULIC TURBINE INDUCER BOOST PUMP
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