NACA Mach Number Indicator for Use in High-Speed Tunnels

reportActive / Technical Report | Accession Number: ADB813529 | Open PDF

Abstract:

Principles of operation of the NACA Mach number indicator are explained, which measures ratio of indicated dynamic pressure to static pressure. The unit performs with efficient accuracy in the NACA 8-foot high-speed tunnel. General design considerations are discussed, and the indicator may also be used to determine local Mach numbers on aerodynamic bodies, and be adapted as a flight Mach number indicator enabling the pilot to read directly his proximity to limiting conditions.

Author(s):
Smith, Norman F.
Author Organization(s):
NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA
Descriptive Note:
Wartime rept.
Pagination:
0020

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release, Document Partially Illegible
Distribution Statement:
Approved For Public Release; Distribution Is Unlimited. Document Partially Illegible.

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
NACA-WR-L-423, NACA-ACR-3G31
Monitor Series:
NACA
 Subject Terms
Joint Capability Areas:
JCA_6.4.1_Secure Information Exchange; JCA_6_Net Centric; JCA_6.4_Information Assurance; JCA_6.1.3_Switching and Routing; JCA_1.3_Human Capital Management; JCA_1_Force Support
Communities of Interest:
Air Platforms
Descriptor(s):
*AERODYNAMICS, *MACHMETERS, MACH NUMBER, WIND TUNNELS
Field(s)/Group(s):
Aerodynamics, Test Facilities, Equipment and Methods
Keyword(s):
ATI 4994, ATI 7936, ATI COLLECTION
Report Date:
1943 Jul 01
Creation Date:
1999 Mar 31