The effects of an inverse-taper leading-edge flap on the aerodynamic characteristics in pitch of a wing-body combination having an aspect ratio of 3 to 45 degrees of sweepback at Mach numbers to 0.92

One of 4,120 reports in the series: NACA Technical Notes available on this site.
Thumbnail image of item number 1 in: 'The effects of an inverse-taper leading-edge flap on the aerodynamic characteristics in pitch of a wing-body combination having an aspect ratio of 3 to 45 degrees of sweepback at Mach numbers to 0.92'.
Thumbnail image of item number 2 in: 'The effects of an inverse-taper leading-edge flap on the aerodynamic characteristics in pitch of a wing-body combination having an aspect ratio of 3 to 45 degrees of sweepback at Mach numbers to 0.92'.
Thumbnail image of item number 3 in: 'The effects of an inverse-taper leading-edge flap on the aerodynamic characteristics in pitch of a wing-body combination having an aspect ratio of 3 to 45 degrees of sweepback at Mach numbers to 0.92'.
Thumbnail image of item number 4 in: 'The effects of an inverse-taper leading-edge flap on the aerodynamic characteristics in pitch of a wing-body combination having an aspect ratio of 3 to 45 degrees of sweepback at Mach numbers to 0.92'.
Showing 1-4 of 58 pages in this report.

PDF Version Also Available for Download.

Description

Report presenting an investigation to determine the effects of an inverse-taper leading-edge flap on the drag and static-longitudinal characteristics of a swept-wing-body combination. Testing was carried out in order to maximize the subsonic lift-drag ratios with minimum penalty to the supersonic capabilities of the airplane. Results regarding drag characteristics and lift and pitching-moment characteristics are provided.

Creation Information

Demele, Fred A. & Powell, K. Harmon August 1958.

Context

This report is part of the collection entitled: National Advisory Committee for Aeronautics Collection and one other and was provided by UNT Libraries Government Documents Department to Digital Library, a digital repository hosted by the UNT Libraries. It has been viewed 73 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: The effects of an inverse-taper leading-edge flap on the aerodynamic characteristics in pitch of a wing-body combination having an aspect ratio of 3 to 45 degrees of sweepback at Mach numbers to 0.92
  • Series Title: NACA Technical Notes

Description

Report presenting an investigation to determine the effects of an inverse-taper leading-edge flap on the drag and static-longitudinal characteristics of a swept-wing-body combination. Testing was carried out in order to maximize the subsonic lift-drag ratios with minimum penalty to the supersonic capabilities of the airplane. Results regarding drag characteristics and lift and pitching-moment characteristics are provided.

Language

Item Type

Identifier

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

  • Accession or Local Control No: 93R14556
  • URL: http://hdl.handle.net/2060/19930085266 External Link
  • Report No.: NACA-TN-4366
  • Center for AeroSpace Information Number: 19930085266
  • Archival Resource Key: ark:/67531/metadc57450

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

This selection of materials from the Technical Report Archive and Image Library (TRAIL) includes hard-to-find reports published by various government agencies. The technical publications contain reports, images, and technical descriptions of research performed for U.S. government agencies. Topics range from mining, desalination, and radiation to broader physics, biology, and chemistry studies. Some reports include maps, foldouts, blueprints, and other oversize materials.

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

  • August 1958

Added to The UNT Digital Library

  • Nov. 17, 2011, 10:13 p.m.

Description Last Updated

  • April 13, 2018, 5:03 p.m.

Usage Statistics

When was this report last used?

Yesterday: 0
Past 30 days: 0
Total Uses: 73
More Statistics

Interact With This Report

Here are some suggestions for what to do next.

Start Reading

Thumbnail image of item number 1 in: 'The effects of an inverse-taper leading-edge flap on the aerodynamic characteristics in pitch of a wing-body combination having an aspect ratio of 3 to 45 degrees of sweepback at Mach numbers to 0.92'.
Thumbnail image of item number 2 in: 'The effects of an inverse-taper leading-edge flap on the aerodynamic characteristics in pitch of a wing-body combination having an aspect ratio of 3 to 45 degrees of sweepback at Mach numbers to 0.92'.
Thumbnail image of item number 3 in: 'The effects of an inverse-taper leading-edge flap on the aerodynamic characteristics in pitch of a wing-body combination having an aspect ratio of 3 to 45 degrees of sweepback at Mach numbers to 0.92'.
Thumbnail image of item number 4 in: 'The effects of an inverse-taper leading-edge flap on the aerodynamic characteristics in pitch of a wing-body combination having an aspect ratio of 3 to 45 degrees of sweepback at Mach numbers to 0.92'.

PDF Version Also Available for Download.

Citations, Rights, Re-Use

Demele, Fred A. & Powell, K. Harmon. The effects of an inverse-taper leading-edge flap on the aerodynamic characteristics in pitch of a wing-body combination having an aspect ratio of 3 to 45 degrees of sweepback at Mach numbers to 0.92, report, August 1958; (digital.library.unt.edu/ark:/67531/metadc57450/: accessed April 24, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.