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Computation Of Unsteady Transonic Flows Through Rotating And Stationary Cascades by Simon Slutsky

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1NASA Contractor Report 2902... Computation Of Unsteady Transonic Flows Through Rotating And Stationary Cascades, III-Acoustic Far-Field Analysis... NASA... November 1977

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NAS 1.26:2902 Digitized from IA1177305-01-0085 .

“NASA Contractor Report 2902... Computation Of Unsteady Transonic Flows Through Rotating And Stationary Cascades, III-Acoustic Far-Field Analysis... NASA... November 1977” Metadata:

  • Title: ➤  NASA Contractor Report 2902... Computation Of Unsteady Transonic Flows Through Rotating And Stationary Cascades, III-Acoustic Far-Field Analysis... NASA... November 1977
  • Author: ➤  
  • Language: English

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The book is available for download in "texts" format, the size of the file-s is: 42.70 Mbs, the file-s for this book were downloaded 80 times, the file-s went public at Thu Jun 30 2022.

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2NASA Technical Reports Server (NTRS) 19780004091: Computation Of Unsteady Transonic Flows Through Rotating And Stationary Cascades. 2: User's Guide To FORTRAN Program B2DATL

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Documentation for the FORTRAN program B2DATL is provided. The program input, output, and operational procedures are described; a dictionary of the principal FORTRAN variables is provided; the function of all subroutines; is outlined and flow charts of the principal subroutines and the main program are presented.

“NASA Technical Reports Server (NTRS) 19780004091: Computation Of Unsteady Transonic Flows Through Rotating And Stationary Cascades. 2: User's Guide To FORTRAN Program B2DATL” Metadata:

  • Title: ➤  NASA Technical Reports Server (NTRS) 19780004091: Computation Of Unsteady Transonic Flows Through Rotating And Stationary Cascades. 2: User's Guide To FORTRAN Program B2DATL
  • Author: ➤  
  • Language: English

“NASA Technical Reports Server (NTRS) 19780004091: Computation Of Unsteady Transonic Flows Through Rotating And Stationary Cascades. 2: User's Guide To FORTRAN Program B2DATL” Subjects and Themes:

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The book is available for download in "texts" format, the size of the file-s is: 60.17 Mbs, the file-s for this book were downloaded 102 times, the file-s went public at Wed Jul 27 2016.

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3NASA Technical Reports Server (NTRS) 19780004092: Computation Of Unsteady Transonic Flows Through Rotating And Stationary Cascades. 3: Acoustic Far-field Analysis

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A small perturbation type analysis has been developed for the acoustic far field in an infinite duct extending upstream and downstream of an axial turbomachinery stage. The analysis is designed to interface with a numerical solution of the near field of the blade rows and, thereby, to provide the necessary closure condition to complete the statement of infinite duct boundary conditions for the subject problem. The present analysis differs from conventional inlet duct analyses in that a simple harmonic time dependence was not assumed, since a transient signal is generated by the numerical near-field solution and periodicity is attained only asymptotically. A description of the computer code developed to carry out the necessary convolutions numerically is included, as well as the results of a sample application using an impulsively initiated harmonic signal.

“NASA Technical Reports Server (NTRS) 19780004092: Computation Of Unsteady Transonic Flows Through Rotating And Stationary Cascades. 3: Acoustic Far-field Analysis” Metadata:

  • Title: ➤  NASA Technical Reports Server (NTRS) 19780004092: Computation Of Unsteady Transonic Flows Through Rotating And Stationary Cascades. 3: Acoustic Far-field Analysis
  • Author: ➤  
  • Language: English

“NASA Technical Reports Server (NTRS) 19780004092: Computation Of Unsteady Transonic Flows Through Rotating And Stationary Cascades. 3: Acoustic Far-field Analysis” Subjects and Themes:

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The book is available for download in "texts" format, the size of the file-s is: 34.71 Mbs, the file-s for this book were downloaded 88 times, the file-s went public at Wed Jul 27 2016.

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4NASA Contractor Report 2900... Computation Of Unsteady Transonic Flows Through Rotating And Stationary Cascades, I - Method Of Analysis... NASA... December 1977

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NAS 1.26:2900 Digitized from IA1177305-01-0082 , IA1177305-01-0083 .

“NASA Contractor Report 2900... Computation Of Unsteady Transonic Flows Through Rotating And Stationary Cascades, I - Method Of Analysis... NASA... December 1977” Metadata:

  • Title: ➤  NASA Contractor Report 2900... Computation Of Unsteady Transonic Flows Through Rotating And Stationary Cascades, I - Method Of Analysis... NASA... December 1977
  • Author: ➤  
  • Language: English

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The book is available for download in "texts" format, the size of the file-s is: 81.87 Mbs, the file-s for this book were downloaded 54 times, the file-s went public at Thu Jun 30 2022.

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5NASA Contractor Report 2901... Computation Of Unsteady Transonic Flows Through Rotating And Stationary Cascades, II-User's Guide To Fortran Program B2DATL... NASA... November 1977

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NAS 1.26:2901 Digitized from IA1177305-01-0084 .

“NASA Contractor Report 2901... Computation Of Unsteady Transonic Flows Through Rotating And Stationary Cascades, II-User's Guide To Fortran Program B2DATL... NASA... November 1977” Metadata:

  • Title: ➤  NASA Contractor Report 2901... Computation Of Unsteady Transonic Flows Through Rotating And Stationary Cascades, II-User's Guide To Fortran Program B2DATL... NASA... November 1977
  • Author: ➤  
  • Language: English

Edition Identifiers:

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The book is available for download in "texts" format, the size of the file-s is: 60.32 Mbs, the file-s for this book were downloaded 55 times, the file-s went public at Thu Jun 30 2022.

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6NASA Technical Reports Server (NTRS) 19780012139: Computation Of Unsteady Transonic Flows Through Rotating And Stationary Cascades. 1: Method Of Analysis

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A numerical method of solution of the inviscid, compressible, two-dimensional unsteady flow on a blade-to-blade stream surface through a stage (rotor and stator) or a single blade row of an axial flow compressor or fan is described. A cyclic procedure has been developed for representation of adjacent blade-to-blade passages which asymptotically achieves the correct phase between all passages of a stage. A shock-capturing finite difference method is employed in the interior of the passage, and a method of characteristics technique is used at the boundaries. The blade slipstreams form two of the passage boundaries and are treated as moving contact surfaces capable of supporting jumps in entropy and tangential velocity. The Kutta condition is imposed by requiring the slipstreams to originate at the trailing edges, which are assumed to be sharp. Results are presented for several transonic fan rotors and compared with available experimental data, consisting of holographic observations of shock structure and pressure contour maps. A subcritical stator solution is also compared with results from a relaxation method. Finally, a periodic solution for a stage consisting of 44 rotor blades and 46 stator blades is discussed.

“NASA Technical Reports Server (NTRS) 19780012139: Computation Of Unsteady Transonic Flows Through Rotating And Stationary Cascades. 1: Method Of Analysis” Metadata:

  • Title: ➤  NASA Technical Reports Server (NTRS) 19780012139: Computation Of Unsteady Transonic Flows Through Rotating And Stationary Cascades. 1: Method Of Analysis
  • Author: ➤  
  • Language: English

“NASA Technical Reports Server (NTRS) 19780012139: Computation Of Unsteady Transonic Flows Through Rotating And Stationary Cascades. 1: Method Of Analysis” Subjects and Themes:

Edition Identifiers:

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The book is available for download in "texts" format, the size of the file-s is: 65.19 Mbs, the file-s for this book were downloaded 76 times, the file-s went public at Thu Jul 28 2016.

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