Effect of Throat Bleed on the Supersonic Performance of a Half-Conical Side-Inlet System Metadata

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Title

  • Main Title Effect of Throat Bleed on the Supersonic Performance of a Half-Conical Side-Inlet System
  • Series Title NACA Research Memorandums

Creator

  • Author: Sitt, Leonard E.
    Creator Type: Personal
  • Author: McKevitt, Frank X.
    Creator Type: Personal
  • Author: Smith, Albert B.
    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: 1956-01-10

Language

  • English

Description

  • Content Description: Memorandum presenting an experimental investigation conducted at Mach numbers 1.5, 1.8, and 2.0 to determine the effects of several throat boundary-layer bleed configurations on the performance of a 25 degree half-conical side-inlet system. The effects of several flush-slot configurations and a porous-surface bleed were determined over ranges of angle of attack and bleed-duct and main-duct mass flow.
  • Physical Description: 32 p. : ill.

Subject

  • Keyword: throat bleed
  • Keyword: aircraft performance
  • Keyword: aircraft inlets

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: 71N70832
  • URL: http://hdl.handle.net/2060/19710065519
  • Report No.: NACA-RM-E55J07
  • Center for AeroSpace Information Number: 19710065519
  • Archival Resource Key: ark:/67531/metadc53193