APPROXIMATE ANALYSIS OF EFFECT ON DRAG OF TRUNCATING THE CONICAL NOSE OF A BODY OF REVOLUTION IN SUPERSONIC FLOW

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1963
Accession Number
AD0400708

Entities

People

  • Neal Tetervin

Organizations

  • Naval Ordnance Laboratory

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aeronautical Engineering
  • Air Force
  • Air Force Facilities
  • Aircrafts
  • Drag
  • Engineering
  • Fluid Dynamics
  • Fluid Mechanics
  • Gas Dynamics
  • Jet Propulsion
  • Mach Number
  • Mechanical Engineering
  • Munitions
  • New York
  • Physics Laboratories
  • Pressure Distribution
  • United States

Technology Areas

  • Hypersonics