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Application of a Channel Design Method to High-solidity Cascades and Tests of an Impulse Cascade with 90° of Turning

A technique is developed for the application of a channel design method to the design of high-solidity cascades with prescribed velocity distributions as a function of arc length along the blade-element profile.

Author : John D. Stanitz

Release : 1952

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File Size : 86.99 MB

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A technique is developed for the application of a channel design method to the design of high-solidity cascades with prescribed velocity distributions as a function of arc length along the blade-element profile. The technique applies to both incompressible and subsonic linearized compressible (ratio of specific heats equal to -1.0), nonviscous, irrotational, fluid motion. An impulse cascade with 90 degree turning was designed for incompressible flow and was tested at the design angle of attack over a range of downstream Mach number from 0.2 to choke flow. To achieve good efficiency, the cascade was designed for prescribed velocities with maximum allowable blade loading according to limitations imposed by considerations of boundary-layer separation.

Technical Note - National Advisory Committee for Aeronautics

APPLICATION OF A CHANNEL DESIGN METHOD TO HIGH - SOLIDITY
CASCADES AND TESTS OF AN IMPULSE CASCADE WITH 90 ° OF TURNING .
John D. Stanitz and Leonard J. Sheldrake . March 1952 . 65p . diagrs . , photos . ,
2 tabs ...

Author : United States. National Advisory Committee for Aeronautics

Release : 1952

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File Size : 23.57 MB

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Report

APPLICATION OF A CHANNEL DESIGN METHOD TO HIGH - SOLIDITY
CASCADES AND TESTS OF AN IMPULSE CASCADE WITH 90° OF TURNING .
John D . Stanitz and Leonard J . Sheldrake . 1953 . ii , 20p . diagrs . , photos . , 2
tabs .

Author : United States. National Advisory Committee for Aeronautics

Release : 1953

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File Size : 50.82 MB

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Annual Report - National Advisory Committee for Aeronautics

APPLICATION OF A CHANNEL DESIGN METHOD TO HIGH - SOLIDITY
CASCADES AND TESTS OF AN IMPULSE CASCADE WITH 90 ° OF TURNING 1
By John D. STANITZ and LEONARD J. SHELDRAKE SUMMARY blade - element
 ...

Author : United States. National Advisory Committee for Aeronautics

Release : 1955

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Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.

Index of NACA Technical Publication

Author : United States. National Advisory Committee for Aeronautics

Release : 1953-06

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File Size : 51.12 MB

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NASA SP.

Stanitz, John D., and Sheldrake, Leonard J.: Application of a Channel Design
Method to HighSolidity Cascades and Tests of an Impulse Cascade with 90° of
Turning. NACA Rep. 1116, 1953. (Supersedes NACA TN 2652.) Ackeret, J. (V. P.
 ...

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Release : 1965

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Research Abstracts and Reclassification Notice

A technique is developed for the application of a channel design method to the
design of high - solidity cascades with ... An impulse cascade with 90° turning
was designed for incompressible flow and was tested at the design angle of
attack ...

Author : United States. National Advisory Committee for Aeronautics

Release : 1951

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File Size : 72.60 MB

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Aeronautical Engineering Review

... ideas you can use with ... ар ELECTRONICS DIVISION Thompson Products ,
Inc. CLEVELAND A. OMO Internal Flow Application of a Channel Design Method
to High - Solidity Cascades and Tests of an Impulse Cascade with 90 ° of Turning
 ...

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Release : 1954

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File Size : 35.48 MB

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The Journal of the Royal Aeronautical Society

Application of a channel design method to high - solidity cascades and tests of an
impulse cascade with 90 ° of turning . J. D. Stanitz and L. J. Sheldrake . N.A.C.A.
Report 1116 ( 1953 ) . A technique is developed for the application of a channel ...

Author : Royal Aeronautical Society

Release : 1954

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File Size : 61.14 MB

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Battelle Technical Review

Application of a Channel Design Method to HighSolidity Cascades and Tests of
an Impulse Cascade With 90 ° of Turning . John D. Stanitz and Leonard J.
Sheldrake . National Advisory Committee for Aeronautics , Technical Note 2652 ,
Mar.

Author : Battelle Memorial Institute

Release : 1952

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File Size : 71.4 MB

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Axial Flow Turbines

Note 2595 ( 1952 ) 136 Stanitz , J . D . , and Sheldrake , L . J . , ' Application of a
Channel Design Method of High Solidity Cascades and Tests of an Impulse
Cascade with 90° of Turning ' , NACĂ Tech . Note 2652 ( 1952 ) Como D . , Apon
 ...

Author : J. H. Horlock

Release : 1966

Publisher : Krieger Publishing Company

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File Size : 87.5 MB

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Cascade Aerodynamics

4 NUMACHI , F . Surface pressure distribution on hydrofoil profiles in cascade . ...
P . W . Practical application of LV systems to aero engine research and
development . AGARD Lect . Ser . 90 ( 1977 ) 10 . ... Application of a channel
design method to high solidity cascades and tests of an impulse cascade with
900 of turning .

Author : J. P. Gostelow

Release : 1984

Publisher : Pergamon

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File Size : 59.79 MB

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Good,No Highlights,No Markup,all pages are intact, Slight Shelfwear,may have the corners slightly dented, may have slight color changes/slightly damaged spine.

Government Reports Announcements

APPLICATION OF A CHANNEL DESIGN METHOD TO HIGH - SOLIDITY
CASCADES AND TESTS OF AN IMPULSE CASCADE WITH 90° OF TURNING ,
by John D . Stanitz and Leonard J . Sheldrake . U . S . National Advisory
Committee for ...

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Release : 1952

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Through-flow Calculations in Axial Turbomachinery

all , design - point selection programs list single variations of inlet angle and inlet
velocity or Mach number with radius for ... level engineering efforts and making
extensive use of expensive computers if turbine performances do not change or if
... Stanitz , John D . , and Sheldrake , Leonard , Application of a Channel Design
Method to High - Solidity Cascades and Tests of an Impulse Cascade with 90° of
 ...

Author : North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Propulsion and Energetics Panel

Release : 1976

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File Size : 66.63 MB

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Aerospace Engineering Index

Author :

Release : 1954

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File Size : 86.47 MB

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The Aeronautical Journal

R . W . Stone , Jr . 2634 - Evaluation of three methods for determining dynamic
characteristics of a turbojet engine . ... 2652 - Application of a channel design
method to high - solidity cascades and tests of an impulse cascade with 90° of
turning ...

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Release : 1952

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Numerical Methods in Laminar and Turbulent Flow

Stanitz , J.D. and Sheldrake , L.J. - Application of a Channel Design Method to
High Solidity Cascades and Tests of an Impulse Cascade with 90 ° of Turning .
NACA Rept . 1116 , 1950 . 12. Hobson , D.C. Shock - Free Transonic Flow in ...

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Release : 1981

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Paper

This figure also gives a plot of the pressure distribution for this blade due to
Denton ' s ( 8 ) direct method . ... LJ " Application of a Channel Design Method to
High - Solidity Cascades and tests of and Impulse Cascade with 90 deg of
Turning " ...

Author :

Release : 1986

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ASME Technical Papers

13 – Inverse calculation of flow in a radial inward flow turbine guide vane
cascade . ... and Sheldrake , L . J . , Application of a channel design method to
high - solidity cascades and tests of an impulse cascade with 90° of turning -
NACA Tech .

Author :

Release : 1984

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File Size : 48.24 MB

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