PRESSURE TEST ON A 0.04-SCALE MODEL OF THE SATURN V LAUNCH VEHICLE AT MACH NUMBERS FROM 1.80 THROUGH 3.00

Abstract

In conjunction with an earlier transonic test, a 0.04-scale model of the Saturn V launch vehicle was tested at Mach numbers from 1.80 to 3.00 for Reynolds number based on model diameter varying from 1.59 to 2.77 million. Static pressure distributions and boundary-layer profiles were measured and are presented herein.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1967
Accession Number
AD0815350

Entities

People

  • J. E. Robertson
  • T. R. Brice

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Boundaries
  • Boundary Layer
  • Dynamic Pressure
  • Free Stream
  • Instrumentation
  • Launch Vehicles
  • Layers
  • Mach Number
  • Measurement
  • Measuring Instruments
  • Models
  • Pressure Distribution
  • Reynolds Number
  • Scale Models
  • Static Pressure
  • Vehicles
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.