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Investigation of two pitot-static tubes at supersonic speeds

Published 2019-06-26 From Legacy CDMS 2 authors
Read paper (PDF) ↗ View on NASA NTRS ↗

Attribution

This is the abstract and citation. Full text lives at NASA NTRS — we link out rather than host. All credit to the authors and Legacy CDMS.

Abstract

Verbatim from NASA NTRS. Not paraphrased, not summarized.

The results of tests at a Mach number of 1.94 of an ogives-nose cylindrical pitot-static tube and similar tests at Mach numbers of 1.93 and 1.62 of a service pitot-static tube to determine body static pressures and indicated Mach numbers are presented and discussed. The radial pressure distribution on the cylindrical bodies is compared with that calculated by an approximate theory.

Authors

  • Hasel, Lowell E
  • Coletti, Donald E

Keywords

  • BODIES - SURFACE CONDITIONS
  • INSTRUMENTS, FLIGHT
  • RESEARCH EQUIPMENT, FREE-FLIGHT
  • FLOW, SUPERSONIC

Citation: Hasel, Lowell E, Coletti, Donald E (2019). Investigation of two pitot-static tubes at supersonic speeds. Legacy CDMS. NASA NTRS ID 19930085521. https://ntrs.nasa.gov/citations/19930085521 ↗