Heat transfer for Mach numbers up to 2.2 and pressure distributions for Mach numbers up to 4.7 from flight investigations of a flat-face-cone and a hemisphere-cone Metadata

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Title

  • Main Title Heat transfer for Mach numbers up to 2.2 and pressure distributions for Mach numbers up to 4.7 from flight investigations of a flat-face-cone and a hemisphere-cone
  • Series Title NACA Research Memorandums

Creator

  • Author: Speegle, Katherine C.
    Creator Type: Personal
  • Author: Chauvin, Leo T.
    Creator Type: Personal
  • Author: Heberlig, Jack C.
    Creator Type: Personal

Contributor

  • Originator: Langley Aeronautical Laboratory
    Contributor Type: Organization
    Contributor Info: National Advisory Committee for Aeronautics. Langley Aeronautical Lab

Date

  • Creation: 1958-05-08

Language

  • English

Description

  • Content Description: Report presenting testing of two blunt-nose models, a flat-face-cone and a hemisphere-cone, at Mach numbers up to 4.7. The main purpose was to determine information about heating rates and transition for different blunt nose shapes for long-range ballistic missiles. Information about pressure measurements and heat transfer is provided.

Subject

  • Keyword: missiles
  • Keyword: blunt noses
  • Keyword: thermodynamics
  • 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: 93R19283
  • URL: http://hdl.handle.net/2060/19930089993
  • Report No.: NACA-RM-L58B18
  • Center for AeroSpace Information Number: 19930089993
  • Archival Resource Key: ark:/67531/metadc63975