An Investigation of Constant Area Supersonic Flow Diffusion

This report has yet to be scanned by Contrails staff

Report Number: ARL 64-81
Author(s): Fejer, Andrew A., Heath, George L., Driftmyer, Richard T.
Corporate Author(s): Research Foundation of the University of Toledo
Laboratory: Aerospace Research Laboratories
Date of Publication: 1964-05
Pages: 66
Contract: AF 33(616)-8271
DoD Project: 7116
DoD Task: 711601
Identifier: AD0603313

Abstract:
Experiments were conducted to determine the nature of the deceleration of supersonic airstreams in straight passages of constant cross sectional area. The magnitude of the losses associated with the recovery of kinetic energy was established, Schlieren observations were made of the field of flow in the passage and the influence of passage length, Mach Number and effective Reynolds Number on maximum obtainable pressure rise were investigated.

Provenance: IIT

Other options for obtaining this report:

Via the Defense Technical Information Center (DTIC):
A record for this report, and possibly a pdf download of the report, exists at DTIC

Via National Technical Report Library:
This report may be available for download from NTRL. Use the Title from this record to locate the item in DTIC Online

Indications of Public Availability
No digital image of an index entry indicating public availability is currently available
The inside cover of this report indicates that it was released for public sale




Export