LANN (Lockheed, AFWAL, NASA-Langley, and NLR) Wing Test Program: Acquisition and Application of Unsteady Transonic Data for Evaluation of Three-Dimensional Computational Methods.

Abstract

This report describes the LANN (Lockheed, AFWAL, NASA-Langley, and NLR) wind tunnel test program. The objective of this program was to acquire a comprehensive experimental data base on a modern, transport type wing in steady and unsteady transonic flow. Details of the model geometry and structural properties are documented. Initial correlations of portions of this data base with numerical results generated by two state-of-the-art computational aerodynamics computer programs are presented. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1983
Accession Number
ADA130701

Entities

People

  • J. B. Malone
  • S. Y. Ruo

Tags

Communities of Interest

  • Air Platforms
  • Space

DTIC Thesaurus Topics

  • Air Force
  • Boundary Layer
  • Computational Fluid Dynamics
  • Computational Science
  • Computer Programs
  • Databases
  • Experimental Data
  • Fluid Dynamics
  • Fluid Flow
  • Geometry
  • Measurement
  • Pressure Distribution
  • Pressure Measurement
  • Test Facilities
  • Three Dimensional
  • Wind Tunnel Tests
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Fluid Mechanics and Fluid Dynamics.
  • Technical Research and Report Writing.