Last edited by Gardaramar
Saturday, July 25, 2020 | History

3 edition of Three-dimensional turbopump flowfield analysis found in the catalog.

Three-dimensional turbopump flowfield analysis

Sharma, O. P.

Three-dimensional turbopump flowfield analysis

final report

by Sharma, O. P.

  • 37 Want to read
  • 7 Currently reading

Published by National Aeronautics and Space Administration, National Technical Information Service, distributor in [Washington, DC], [Springfield, Va .
Written in English

    Subjects:
  • Fluid dynamics.

  • Edition Notes

    Other titlesThree dimensional turbopump flowfield analysis.
    StatementO.P. Sharma, K.A. Belford and R.H. Ni.
    SeriesNASA-CR -- 190978., NASA contractor report -- NASA CR-190978.
    ContributionsBelford, K. A., Ni, R. H., United States. National Aeronautics and Space Administration.
    The Physical Object
    FormatMicroform
    Pagination1 v. (various pagings)
    ID Numbers
    Open LibraryOL14685872M


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Three-dimensional turbopump flowfield analysis by Sharma, O. P. Download PDF EPUB FB2

Three-Dimensional Turbopump Flowfield Analysis Final Report i O. R Sharma, K. Belford and R. Ni United Technologies Corporation Pratt & Whitney Commercial Engineering Ap Prepared for George C.

Marshall Space Flight Center National Aeronautics and Space Administration Marshall Space Flight Center, AL Under Contract NAS Get this from a library. Three-dimensional turbopump flowfield analysis: final report. [O P Sharma; K A Belford; R H Ni; United States.

National Aeronautics and Space Administration.]. One, Two and Three Dimensional Flows. Term one, two or three dimensional flow refers to the number of space coordinated required to describe a flow.

It appears that any physical flow is generally three-dimensional. But these are difficult to calculate and call for as much simplification as possible.

A critical speed analysis is performed for a ton thrust demonstrator turbopump considering the casing structural flexibility.

A full three-dimensional finite-element method including rotor and. @article{osti_, title = {Space shuttle main engine high pressure fuel turbopump turbine blade cracking}, author = {Lee, H.}, abstractNote = {The analytical results from two-dimensional (2D) and three-dimensional (3D) finite element model investigations into the cracking of Space Shuttle Main Engine (SSME) High Pressure Fuel Turbopump (HPFTP) first- and second-stage turbine blades are.

Dimensional Analysis 29 a b Figure Ellipse. The general formula is then A = X α fαa αb2−α, () where fα is the coefficient of the term with aα in it.

This representa-tion is not a fruitful way to think about area. Suppose, for example, that the correct function is A = (a2 + b2)/(a + b).

This relatively.