Published September 1973
| Version v1
Report
Restricted
Summary of wind tunnel determined aerodynamic coefficients for the 155 MM XM549 projectile configuration
Description
no abstract available
Availability note (English)
MF available from INIS under the Report Number.
Files
Restricted
The record is publicly accessible, but files are restricted to users with access.
Additional details
Publishing Information
- Imprint Pagination
- 41 p.
- Report number
- SLA--73-607
INIS
- Country of Publication
- United States
- Country of Input or Organization
- United States
- INIS RN
- 5098152
- Subject category
- S42: ENGINEERING; S42: ENGINEERING;
- Descriptors DEI
- AERODYNAMICS; CONFIGURATION; MACH NUMBER; MISSILES; NUCLEAR WEAPONS; SUBSONIC FLOW; SUPERSONIC FLOW; TESTING; TRANSONIC FLOW; WIND TUNNELS
- Descriptors DEC
- FLUID FLOW; FLUID MECHANICS; MECHANICS; TUNNELS; VELOCITY