Comparison of several methods of predicting the pressure loss at altitude across a baffled aircraft-engine cylinder

One of 1,423 reports in the series: NACA Technical Reports available on this site.
Thumbnail image of item number 1 in: 'Comparison of several methods of predicting the pressure loss at altitude across a baffled aircraft-engine cylinder'.
Thumbnail image of item number 2 in: 'Comparison of several methods of predicting the pressure loss at altitude across a baffled aircraft-engine cylinder'.
Thumbnail image of item number 3 in: 'Comparison of several methods of predicting the pressure loss at altitude across a baffled aircraft-engine cylinder'.
Thumbnail image of item number 4 in: 'Comparison of several methods of predicting the pressure loss at altitude across a baffled aircraft-engine cylinder'.
Showing 1-4 of 15 pages in this report.

PDF Version Also Available for Download.

Description

Several methods of predicting the compressible-flow pressure loss across a baffled aircraft-engine cylinder were analytically related and were experimentally investigated on a typical air-cooled aircraft-engine cylinder. Tests with and without heat transfer covered a wide range of cooling-air flows and simulated altitudes from sea level to 40,000 feet. Both the analysis and the test results showed that the method based on the density determined by the static pressure and the stagnation temperature at the baffle exit gave results comparable with those obtained from methods derived by one-dimensional-flow theory. The method based on a characteristic Mach number, although related analytically to … continued below

Physical Description

375 - 389 p. : ill.

Creation Information

Neustein, Joseph & Schafer, Louis J., Jr. October 9, 1945.

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 163 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.

Authors

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: Comparison of several methods of predicting the pressure loss at altitude across a baffled aircraft-engine cylinder
  • Series Title: NACA Technical Reports

Description

Several methods of predicting the compressible-flow pressure loss across a baffled aircraft-engine cylinder were analytically related and were experimentally investigated on a typical air-cooled aircraft-engine cylinder. Tests with and without heat transfer covered a wide range of cooling-air flows and simulated altitudes from sea level to 40,000 feet. Both the analysis and the test results showed that the method based on the density determined by the static pressure and the stagnation temperature at the baffle exit gave results comparable with those obtained from methods derived by one-dimensional-flow theory. The method based on a characteristic Mach number, although related analytically to one-dimensional-flow theory, was found impractical in the present tests because of the difficulty encountered in defining the proper characteristic state of the cooling air. Accurate predictions of altitude pressure loss can apparently be made by these methods, provided that they are based on the results of sea-level tests with heat transfer.

Physical Description

375 - 389 p. : ill.

Language

Item Type

Identifier

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

  • Accession or Local Control No: 93R21220
  • URL: http://hdl.handle.net/2060/19930091930 External Link
  • Report No.: NACA-TR-858
  • Center for AeroSpace Information Number: 19930091930
  • Archival Resource Key: ark:/67531/metadc60153

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 9, 1945

Added to The UNT Digital Library

  • Nov. 17, 2011, 5:13 p.m.

Description Last Updated

  • April 9, 2018, 2:26 p.m.

Usage Statistics

When was this report last used?

Yesterday: 0
Past 30 days: 0
Total Uses: 163
More Statistics

Interact With This Report

Here are some suggestions for what to do next.

Start Reading

Thumbnail image of item number 1 in: 'Comparison of several methods of predicting the pressure loss at altitude across a baffled aircraft-engine cylinder'.
Thumbnail image of item number 2 in: 'Comparison of several methods of predicting the pressure loss at altitude across a baffled aircraft-engine cylinder'.
Thumbnail image of item number 3 in: 'Comparison of several methods of predicting the pressure loss at altitude across a baffled aircraft-engine cylinder'.
Thumbnail image of item number 4 in: 'Comparison of several methods of predicting the pressure loss at altitude across a baffled aircraft-engine cylinder'.

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

Neustein, Joseph & Schafer, Louis J., Jr. Comparison of several methods of predicting the pressure loss at altitude across a baffled aircraft-engine cylinder, report, October 9, 1945; (https://digital.library.unt.edu/ark:/67531/metadc60153/: accessed June 7, 2026), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.

Back to Top of Screen