Flow Phenomena in Starting a Hypersonic Shock Tunnel

Item

Title
Flow Phenomena in Starting a Hypersonic Shock Tunnel
Date
1955
Index Abstract
Online
Photo Quality
Undetermined
Report Number
AEDC TN 55-16
Creator
Glick, H. S.
Hertzberg, A.
Smith, W. E.
Corporate Author
Cornell Aeronautical Lab, Inc.
Extent
8
PB Number
PB118114
Identifier
AD0056231
Access Rights
Unknown
Distribution Classification
2
DTIC Record Exists
No
Distribution Change Authority Correspondence
None
Distribution Conflict
Yes
Index Price
$4.80
Report Availability
Not available via Contrails
Date Issued
1955-03
Abstract
The abstract for this report is either unavailable or has yet to be entered
Index In
U.S. Government Research Reports
Type
report