Accession Number:

AD0658995

Title:

WIND TUNNEL TEST STUDY

Descriptive Note:

Final engineering rept. (Part 1), 25 Jan-1 Apr 1958

Corporate Author:

CHRYSLER CORP CENTER LINE MI WARREN DEFENSE DIV

Personal Author(s):

Report Date:

1958-06-01

Pagination or Media Count:

85.0

Abstract:

The report includes information pertaining to the construction and testing of the CARV Chrysler Aerial Research Vehicle. This wind tunnel test model was constructed and tested. The first part of the test program covered the following investigations a Vane effectiveness in hovering. b Forward flight conditions for tandem configuration. c Forward flight conditions for abreast configuration. d Finding a method to reduce the positive pitching moment.

Subject Categories:

  • Aerodynamics
  • Test Facilities, Equipment and Methods
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE