Accession Number:

AD0736825

Title:

Wind Tunnel Test of the Aerodynamics and Dynamics of Rotor Spinup, Stopping and Folding on a Semispan Folding Tilt-Rotor Model. Volume VII

Descriptive Note:

Final rept. Jan-Jul 1971

Corporate Author:

BOEING VERTOL CO PHILADELPHIA PA

Report Date:

1971-10-01

Pagination or Media Count:

402.0

Abstract:

Wind tunnel test data obtained with a 19-scale semispan, unpowered, dynamically-scaled Model 213 stowedtilt rotor are reported. The objectives of the tests were to obtain aerodynamic, structural, and dynamics data during the spinup, feather and blade fold cycles of this vehicle.

Subject Categories:

  • VSTOL

Distribution Statement:

APPROVED FOR PUBLIC RELEASE