Comparison at supersonic speeds of translating spike inlets having blunt- and sharp-lip cowls Metadata

Metadata describes a digital item, providing (if known) such information as creator, publisher, contents, size, relationship to other resources, and more. Metadata may also contain "preservation" components that help us to maintain the integrity of digital files over time.

Title

  • Main Title Comparison at supersonic speeds of translating spike inlets having blunt- and sharp-lip cowls
  • Series Title NACA Research Memorandums

Creator

  • Author: Gorton, Gerald C.
    Creator Type: Personal
  • Author: Dryer, Murray
    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: 1954-01-19

Language

  • English

Description

  • Content Description: Report presenting an investigation of two translating spike inlets with blunt- and sharp-lip cowls in the supersonic wind tunnel at a range of free-stream Mach numbers and angles of attack. Results regarding the inlet stability, critical inlet performance at zero angle of attack, and inlet-engine matching are provided.
  • Physical Description: 37 p. : ill.

Subject

  • Keyword: aircraft inlets
  • Keyword: aircraft cowling

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: 93R19803
  • URL: http://hdl.handle.net/2060/19930090513
  • Report No.: NACA-RM-E54J07
  • Center for AeroSpace Information Number: 19930090513
  • Archival Resource Key: ark:/67531/metadc64825