Characteristics of Low-Aspect-Ratio Wings at Supercritical Mach Numbers,

Abstract

NO ABSTRACT DUE TO ILLEGIBILITY OF REPORT (KAR)

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1949
Accession Number
ADA298292

Entities

People

  • John Stack
  • W. F. Lindsey

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aeronautics
  • Aircrafts
  • Aspect Ratio
  • Boundary Layer
  • Civil Aviation
  • Coefficients
  • Dynamic Pressure
  • Errors
  • Flow
  • Mach Number
  • Pressure Gradients
  • Reynolds Number
  • Shape
  • Shock
  • Static Pressure
  • Two Dimensional