U.S. Army Helicopter Design Datcom Volume 1. Airfoils

Abstract

This report contains airfoil data of interest for rotor applications. The data is presented in the form of lift, drag, and pitching moment coefficients and, in most cases, it covers the complete Mach number range from low subsonic to supercritical flow conditions. An introductory section presents airfoil data trends and information pertaining to the source and usefulness of such data.

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Document Details

Document Type
Technical Report
Publication Date
May 31, 1976
Accession Number
ADA033425

Entities

People

  • L. U. Dadone

Organizations

  • Boeing Rotorcraft Systems

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aircrafts
  • Airframes
  • Boundary Layer
  • Computational Fluid Dynamics
  • Dynamic Pressure
  • Fixed Wing Aircraft
  • Flow Visualization
  • Fluid Dynamics
  • Fluid Flow
  • Geometry
  • Helicopters
  • Mach Number
  • Measurement
  • Pressure Distribution
  • Wind Tunnel Tests
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Library and Information Science