Accession Number:

AD0647693

Title:

INVESTIGATION OF THE UTILITY OF LOW SPEED DYNAMIC MODEL TESTS FOR AIRCRAFT STORE LAUNCH RESEARCH,

Descriptive Note:

Test rept.,

Corporate Author:

DAVID TAYLOR MODEL BASIN WASHINGTON D C AERODYNAMICS LAB

Personal Author(s):

Report Date:

1967-01-01

Pagination or Media Count:

48.0

Abstract:

Results of a study to determine the utility of using a low-speed wind tunnel and a statistical approach for aircraft-store separations research are presented. An A-4E aircraft model and a Mark 88 Mod 0 practice bomb, dynamically and geometrically scaled to 10 percent, were used in the test. Multiple exposure photographs of each drop were made and transparent overlay grids were used to read store displacements and pitch angles from the photographs. Smooth trajectory curves were obtained, indicating that a sufficient number of drops were made to obtain a good average. Author

Subject Categories:

  • Test Facilities, Equipment and Methods
  • Fire Control and Bombing Systems

Distribution Statement:

APPROVED FOR PUBLIC RELEASE