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Investigation of two pitot-static tubes at supersonic speeds

NASA NTRS · Other · 19930085521 · Published 2019-06-26 · Legacy CDMS · 2 authors

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Abstract and citation only, verbatim from NASA NTRS; full text lives there. All credit to the authors and Legacy CDMS.

Abstract

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 ↗