A wind tunnel investigation of jets exhausting into a crossflow.
Volume 4,
Additional data for three-jet configuration /
L.B. Fricke, P.T. Wooler, H. Ziegler.
Description
- Language(s)
-
English
- Published
-
Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970.
- Summary
-
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.
- Note
-
"This report presents the results of Contract F33615-69-C-1602, Project No. 698BT."
"Northrop Corporation, Aircraft Division.
"December 1970."
- Physical Description
-
vi, 191 pages :
illustrations, figures ;
28 cm.
Viewability