Experimental investigation at supersonic speeds of twin-scoop duct inlets of equal area 3: inlet enclosing 37.2 percent of the maximum circumference of the forebody Metadata

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Title

  • Main Title Experimental investigation at supersonic speeds of twin-scoop duct inlets of equal area 3: inlet enclosing 37.2 percent of the maximum circumference of the forebody
  • Series Title NACA Research Memorandums

Creator

  • Author: Davis, Wallace F.
    Creator Type: Personal
  • Author: Edwards, Sherman S.
    Creator Type: Personal

Contributor

  • Originator: Ames Aeronautical Laboratory (U.S.)
    Contributor Type: Organization
    Contributor Info: National Advisory Committee for Aeronautics. Ames Aeronautical Lab

Date

  • Creation: 1948-07-22

Language

  • English

Description

  • Content Description: Report presenting testing of a twin-scoop duct inlet that enclosed 37.2 percent of the forebody circumference at Mach numbers between 1.36 and 2.01. The approach to each scoop consisted of a ramp that deflected the flow to create an oblique shock wave in front of the duct entrance. Results regarding the inlet proportions, ramp angle, slots, and angle of incidence are provided.
  • Physical Description: 25 p. : ill.

Subject

  • Keyword: scoop duct inlets
  • Keyword: aerodynamics

Collection

  • Name: National Advisory Committee for Aeronautics Collection
    Code: NACA
  • Name: Technical Report Archive and Image Library
    Code: TRAIL

Institution

  • Name: UNT Libraries Government Documents Department
    Code: UNTGD

Rights

  • Rights Access: public
  • Rights License: pd
  • Rights Statement: No Copyright, Unclassified, Unlimited, Publicly available

Resource Type

  • Report

Format

  • Text

Identifier

  • Accession or Local Control No: 93R14746
  • URL: http://hdl.handle.net/2060/19930085456
  • Report No.: NACA-RM-A8E04
  • Center for AeroSpace Information Number: 19930085456
  • Archival Resource Key: ark:/67531/metadc57767

Note

  • Display Note: "III."
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