ONE-FIFTH SCALE INLET MODEL WIND TUNNEL TEST REPORT, VOLUME 3

Abstract

Tabulated data are presented for the high speed tests (Mach 0.4 to 0. 85).

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1965
Accession Number
AD0647396

Entities

Organizations

  • General Electric

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Flow
  • Aircrafts
  • Army Aviation
  • Boundary Layer
  • Dynamic Pressure
  • Flow
  • Free Stream
  • Government Procurement
  • Governments
  • Instrumentation
  • Mach Number
  • Recording Systems
  • Research Aircraft
  • Scale Models
  • Static Pressure
  • Wind Tunnel Tests
  • Wind Tunnels

Fields of Study

  • Physics