AERODYNAMIC CHARACTERISTICS OF WINGS AT SUPERSONIC SPEEDS,

Abstract

Contents: Application of Busemann's Conical Field Method to Thin Wings, Aerodynamic Characteristics of Solid Rectangular Airfoils at Supersonic Speeds, by E. A. Bonney; The Reverse Delta Planform; Lift and Drag Characteristics of Delta Wings at Supersonic Speeds, by E. A. Bonney; and Sectional Characteristics of Standard Airfoils, by E. A. Bonney.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1947
Accession Number
AD0634865

Entities

People

  • E. A. Bonney
  • R. M. Snow

Organizations

  • Johns Hopkins University Applied Physics Laboratory

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aspect Ratio
  • Delta Wings
  • Dynamic Pressure
  • Equations
  • Free Stream
  • Geometry
  • Leading Edges
  • Mach Number
  • Physics Laboratories
  • Pressure Distribution
  • Skin Friction
  • Supersonic Flow
  • Swept Wings
  • Thin Wings
  • Trailing Edges
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow