Methods of Approximating Inviscid Jet Boundaries for Highly Underexpanded Supersonic Nozzles

Item

Title
Methods of Approximating Inviscid Jet Boundaries for Highly Underexpanded Supersonic Nozzles
Date
1962
Index Abstract
Coming Soon
Photo Quality
Undetermined
Report Number
AEDC TDR 62-7
Creator
Henson, J. R.
Robertson, J. E.
Corporate Author
Arnold Engineering Development Center
Laboratory
Arnold Engineering Development Center
Extent
63
Identifier
AD0275641
Access Rights
Unknown
Distribution Classification
1
Contract
AF 40(600)-800
DTIC Record Exists
Yes
Distribution Change Authority Correspondence
None
Distribution Conflict
No
Abstract
Methods of approximating inviscid boundaries of jets exhausting from axisymmetric supersonic nozzles into a quiescent atmosphere and moving streams have been developed. Jet shapes from two typical afterbody configurations were calculated for various flight conditions. Good agreement with available theoretical and experimental data was obtained. A step-by-step calculational procedure is given in the Appendix.
The abstract for this report is either unavailable or has yet to be entered
Report Availability
Not available via Contrails
Date Issued
1962-05
Publisher
Arnold Air Force Station, TN : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force
Index In
DTIC
Type
report