Accession Number:

AD0720232

Title:

A Wind Tunnel Investigation of Jets Exhausting into a Crossflow. Volume II. Additional Data for the One-Jet Configuration.

Descriptive Note:

Technical rept.,

Corporate Author:

NORTHROP CORP HAWTHORNE CALIF AIRCRAFT DIV

Report Date:

1970-12-01

Pagination or Media Count:

506.0

Abstract:

A low speed wind tunnel test of a four-foot diameter circular plate model was conducted to determine surface static pressure distributions jet paths, and jet decay characteristics in the presence of a crossflow. Data were obtained for a one-jet configuration with the jet exiting at a number of angles to the plate and at various velocity ratios and sideslip angles. The report is the second of four volumes. The test model, instrumentation, test procedure, and reduction and accuracy of the test data were discussed in Volume 1. Author

Subject Categories:

  • Aerodynamics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE