columbus · Design And Testing Of An Axisymmetric Hypersonic Nozzle For A Low Density Wind Tunnel

Design And Testing Of An Axisymmetric Hypersonic Nozzle For A Low Density Wind Tunnel

Title: Design And Testing Of An Axisymmetric Hypersonic Nozzle For A Low Density Wind Tunnel
Date: 1956
Index Abstract: Limited
Photo Quality: Incomplete
Report Number: WADC TR 56-341
Corporate Author: University of California
Laboratory: Aeronautical Research Laboratory
Extent: 95
PB Number: PB125081
Identifier: AD0097178
Access Rights: ASTIA
Distribution Classification: 2
Contract: AF 33(616)-418
DoD Task: 70134
DTIC Record Exists: No
Distribution Change Authority Correspondence: None
Distribution Conflict: Yes
Report Availability: Not available via Contrails
Date Issued: 1956-08
DoD Project: 1363 - Wind Tunnel Studies
Abstract: The abstract for this report is either unavailable or has yet to be entered
Provenance: IIT
Type: report