NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

The auto‑search feature has been disabled based on user feedback. Enter a search term/phrase and click “Search” to begin.

Back to Results
Investigation of two pitot-static tubes at supersonic speedsThe 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.
Document ID
19930085521
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Hasel, Lowell E
Coletti, Donald E
Date Acquired
August 16, 2013
Publication Date
November 19, 1948
Report/Patent Number
NACA-RM-L8I02
Report Number: NACA-RM-L8I02
Accession Number
93R14811
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
BODIES - SURFACE CONDITIONS
INSTRUMENTS, FLIGHT
RESEARCH EQUIPMENT, FREE-FLIGHT
FLOW, SUPERSONIC

Related Records

There are no records associated with this record.
No Preview Available