Investigation at supersonic speeds of an inlet employing conical flow separation from a probe ahead of a blunt body Metadata

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Title

  • Main Title Investigation at supersonic speeds of an inlet employing conical flow separation from a probe ahead of a blunt body
  • Series Title NACA Research Memorandums

Creator

  • Author: Hearth, Donald P.
    Creator Type: Personal
  • Author: Gorton, Gerald C.
    Creator Type: Personal

Contributor

  • Originator: Lewis Flight Propulsion Laboratory
    Contributor Type: Organization
    Contributor Info: National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab

Date

  • Creation: 1953-01-19

Language

  • English

Description

  • Content Description: Report presenting an investigation in the supersonic wind tunnel on an inlet employing conical flow separation from a probe extending upstream from a hemispherical-nosed centerbody. Pressure-recovery and drag characteristics for the inlet were very nearly comparable with a conical-spike inlet, but compared less favorably at Mach numbers below 2.0. A large reduction in pressure recovery and mass flow was obtained at angle of attack.
  • Physical Description: 32 p. : ill.

Subject

  • Keyword: aircraft inlets
  • Keyword: flow separation

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: 93R16758
  • URL: http://hdl.handle.net/2060/19930087468
  • Report No.: NACA-RM-E52K18
  • Center for AeroSpace Information Number: 19930087468
  • Archival Resource Key: ark:/67531/metadc59520