Accession Number:

AD0912860

Title:

Variable Camber Wing.

Descriptive Note:

Progress rept. no. 4, For Period Ending 15 Aug 73.

Corporate Author:

BOEING AEROSPACE CO SEATTLE WA

Personal Author(s):

Report Date:

1973-08-15

Pagination or Media Count:

8.0

Abstract:

This report outlines progress in the following areas 1 The calculated airplane performance comparisons indicate that the advanced technology variable camber wing offers substantial performance improvements at low speed, loiter, cruise, and combat conditions 2 A flight control system has defined that provides the required level of safety and flying qualities 3 Flap loads, freeplay and stiffness requirements, Structural element design, Skin sizes and actuator sizes have been developed and 4 Leading and trailing edge flap design layouts have been prepared.

Subject Categories:

  • Attack and Fighter Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE