Accession Number:

AD0658498

Title:

THE STATIC AERODYNAMIC CHARACTERISTICS OF A VARIABLE SWEEP WING RESEARCH MODEL.

Descriptive Note:

Test rept.,

Corporate Author:

DAVID TAYLOR MODEL BASIN WASHINGTON D C AERODYNAMICS LAB

Personal Author(s):

Report Date:

1967-03-01

Pagination or Media Count:

64.0

Abstract:

A wind tunnel study was conducted to determine the effect of Mach number, angle of attack, and wing sweep angle on the longitudinal aerodynamic characteristics of a variable sweep wing research model. The study was conducted at Mach numbers between 0.60 and 1.15 and at angles of attack from -2 to 16 degrees. The report presents the data for the static phase of the investigation. Author

Subject Categories:

  • Aircraft
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE