Accession Number:

AD0729429

Title:

Design Studies and Model Tests of the Stowed Tilt Rotor Concept. Volume III. Appendixes

Descriptive Note:

Research and development technical rept.

Corporate Author:

BOEING VERTOL CO PHILADELPHIA PA

Personal Author(s):

Report Date:

1971-07-01

Pagination or Media Count:

163.0

Abstract:

This Appendix contains a description of the drag prediction methodology used in this study, minimum parasite drag breakdowns for all the point design aircraft, and detailed performance data for the Design Point 1, 2, and 3 aircraft.

Subject Categories:

  • VSTOL

Distribution Statement:

APPROVED FOR PUBLIC RELEASE