Accession Number:

AD0903840

Title:

Pressure Distributions on a Delta Wing Horizontal Stabilizer Combination at Mach Numbers from 0.3 to 2.9. Volume 11. Vertical tail section and Total Surface Aerodynamic Coefficients, Chordwise Pressure Distributions.

Descriptive Note:

Final rept. on Task 3,

Corporate Author:

BOEING COMMERCIAL AIRPLANE CO SEATTLE WA

Report Date:

1972-07-15

Pagination or Media Count:

408.0

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 integrated section and total surface characteristics and local surface chordwise pressure distributions for the vertical tail.

Subject Categories:

  • Aerodynamics
  • Transport Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE