Accession Number:

ADA088272

Title:

Pressure and Heat Transfer Measurements on Large Indented Nosetips.

Descriptive Note:

Final rept.,

Corporate Author:

NAVAL SURFACE WEAPONS CENTER SILVER SPRING MD

Report Date:

1979-06-01

Pagination or Media Count:

124.0

Abstract:

This report presents pressure and heat transfer data for 4 indented nosetip shapes. The tests were conducted in the NSWC Hypersonic Tunnel at Mach numbers 5 and 6. The report also presents an instrumentation technique developed as a result of a structural failure of one of the indented nosetip models. Author

Subject Categories:

  • Test Facilities, Equipment and Methods
  • Guided Missile Warheads and Fuzes
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE