Accession Number:

ADA175951

Title:

Surface Pressure Measurements on a Double Delta Wing/Body Configuration at Mach 2 and Mach 3 (WTR 1396).

Descriptive Note:

Wind tunnel data rept. 25 Feb-1 Mar 84,

Corporate Author:

NAVAL SURFACE WEAPONS CENTER SILVER SPRING MD

Personal Author(s):

Report Date:

1986-06-01

Pagination or Media Count:

102.0

Abstract:

The surface pressures on a clipped double-delta wingbody configuration were measured at Mach 2 and Mach 3 in the NSWC Supersonic Tunnel Number Two at angles-of-attack up to 20 deg. The winged-body model configuration has a 2-inch diameter body consisting of a 3-caliber tangent-ogive nose and and a 7-caliber cylindrical afterbody. The wing was a clipped double-delta configuration. The body had 91 pressure taps located at various axial and circumferential locations, and the wing had 47. Surface pressures were measured at several angles-of-attack for various model roll positions at both Mach 2 and Mach 3. Keywords Double delta wing Wing body configuration High angle-of-attack aerodynamics.

Subject Categories:

  • Test Facilities, Equipment and Methods
  • Guided Missile Dynamics, Configurations and Control Surfaces
  • Guided Missiles

Distribution Statement:

APPROVED FOR PUBLIC RELEASE