Accession Number:

AD0903834

Title:

Pressure Distributions on a Delta Wing - Horizontal Stabilizer Combination at Mach Numbers from 0.3 to 2.9. Volume 6. Wing Chordwise Pressure Distribution - Nacelles Off.

Descriptive Note:

Final rept. on Task 3,

Corporate Author:

BOEING COMMERCIAL AIRPLANE CO SEATTLE WA

Report Date:

1972-07-15

Pagination or Media Count:

390.0

Abstract:

This report presents the results of wind tunnel pressure distribution measurements made on a model of the Boeing supersonic transport configuration during design of the prototype airplanes. This volume contains wing upper and lower surface chordwise pressure distributions for the nacelles-off configuration.

Subject Categories:

  • Aerodynamics
  • Transport Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE