Method of designing cascade blades with prescribed velocity distributions in compressible potential flows

One of 1,423 reports in the series: NACA Technical Reports available on this site.
Thumbnail image of item number 1 in: 'Method of designing cascade blades with prescribed velocity distributions in compressible potential flows'.
Thumbnail image of item number 2 in: 'Method of designing cascade blades with prescribed velocity distributions in compressible potential flows'.
Thumbnail image of item number 3 in: 'Method of designing cascade blades with prescribed velocity distributions in compressible potential flows'.
Thumbnail image of item number 4 in: 'Method of designing cascade blades with prescribed velocity distributions in compressible potential flows'.
Showing 1-4 of 11 pages in this report.

PDF Version Also Available for Download.

Description

By use of the assumption that the pressure-volume relation is linear, a solution to the problem of designing a cascade for a given turning and with a prescribed velocity distribution along the blade in a potential flow of a compressible perfect fluid was obtained by a method of correspondence between potential flows of compressible and incompressible fluids. The designing of an isolated airfoil with a prescribed velocity distribution along the airfoil is considered as a special case of cascade. If the prescribed velocity distribution is not theoretically attainable, the method provides a means of modifying the distribution so as to … continued below

Physical Description

559 - 569 p.

Creation Information

Costello, George R. October 1, 1949.

Context

This report is part of the collection entitled: National Advisory Committee for Aeronautics Collection and was provided by the UNT Libraries Government Documents Department to the UNT Digital Library, a digital repository hosted by the UNT Libraries. It has been viewed 164 times. More information about this report can be viewed below.

Who

People and organizations associated with either the creation of this report or its content.

Author

Originator

Provided By

UNT Libraries Government Documents Department

Serving as both a federal and a state depository library, the UNT Libraries Government Documents Department maintains millions of items in a variety of formats. The department is a member of the FDLP Content Partnerships Program and an Affiliated Archive of the National Archives.

About | Browse this Partner

Contact Us

Corrections Questions

What

Descriptive information to help identify this report. Follow the links below to find similar items on the Digital Library.

Titles

  • Main Title: Method of designing cascade blades with prescribed velocity distributions in compressible potential flows
  • Series Title: NACA Technical Reports

Description

By use of the assumption that the pressure-volume relation is linear, a solution to the problem of designing a cascade for a given turning and with a prescribed velocity distribution along the blade in a potential flow of a compressible perfect fluid was obtained by a method of correspondence between potential flows of compressible and incompressible fluids. The designing of an isolated airfoil with a prescribed velocity distribution along the airfoil is considered as a special case of cascade. If the prescribed velocity distribution is not theoretically attainable, the method provides a means of modifying the distribution so as to obtain a physically significant blade shape. Numerical examples are included.

Physical Description

559 - 569 p.

Language

Item Type

Identifier

Unique identifying numbers for this report in the Digital Library or other systems.

  • Accession or Local Control No: 93R21329
  • URL: http://hdl.handle.net/2060/19930092039 External Link
  • Report No.: NACA-TR-978
  • Center for AeroSpace Information Number: 19930092039
  • Archival Resource Key: ark:/67531/metadc60315

Collections

This report is part of the following collections of related materials.

National Advisory Committee for Aeronautics Collection

The National Advisory Committee for Aeronautics (NACA) was a U.S. federal agency founded on March 3, 1915 to undertake, promote, and institutionalize aeronautical research. On October 1, 1958 the agency was dissolved, and its assets and personnel transferred to the newly created National Aeronautics and Space Administration (NASA).

About | Browse this Collection

Technical Report Archive and Image Library

The Technical Report Archive & Image Library (TRAIL) identifies, acquires, catalogs, digitizes and provides unrestricted access to U.S. government agency technical reports. The mission of TRAIL is to ensure preservation, discoverability, and persistent open access to government technical publications regardless of form or format.

About | Browse this Collection

What responsibilities do I have when using this report?

Digital Files

When

Dates and time periods associated with this report.

Creation Date

  • October 1, 1949

Added to The UNT Digital Library

  • Nov. 17, 2011, 5:13 p.m.

Description Last Updated

  • April 2, 2018, 8:09 p.m.

Usage Statistics

When was this report last used?

Yesterday: 0
Past 30 days: 0
Total Uses: 164
More Statistics

Interact With This Report

Here are some suggestions for what to do next.

Start Reading

Thumbnail image of item number 1 in: 'Method of designing cascade blades with prescribed velocity distributions in compressible potential flows'.
Thumbnail image of item number 2 in: 'Method of designing cascade blades with prescribed velocity distributions in compressible potential flows'.
Thumbnail image of item number 3 in: 'Method of designing cascade blades with prescribed velocity distributions in compressible potential flows'.
Thumbnail image of item number 4 in: 'Method of designing cascade blades with prescribed velocity distributions in compressible potential flows'.

PDF Version Also Available for Download.

Citations, Rights, Re-Use

International Image Interoperability Framework

IIF Logo

We support the IIIF Presentation API

Links for Robots

Helpful links in machine-readable formats.

Archival Resource Key (ARK)

International Image Interoperability Framework (IIIF)

Metadata Formats

Images

URLs

Stats

Costello, George R. Method of designing cascade blades with prescribed velocity distributions in compressible potential flows, report, October 1, 1949; (https://digital.library.unt.edu/ark:/67531/metadc60315/: accessed April 25, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.

Back to Top of Screen