Accession Number:

AD0092663

Title:

AN EXPERIMENTAL STUDY AT HIGH SUBSONIC SPEEDS OF SEVERAL TAIL CONFIGURATIONS ON A MODEL WITH AN UNSWEPT WING

Descriptive Note:

Research memorandum

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON DC

Personal Author(s):

Report Date:

1956-04-04

Pagination or Media Count:

72.0

Abstract:

Subject Categories:

  • Aerodynamics
  • Aircraft
  • Guided Missile Dynamics, Configurations and Control Surfaces

Distribution Statement:

APPROVED FOR PUBLIC RELEASE