Flow Calibration of the Laser Test Shelter Airflow Duct.

reportActive / Technical Report | Accession Number: ADA042187 | Open PDF

Abstract:

This report documents an experimental flow field mapping conducted in the airflow duct of the laserfuelsairflow facility. Velocity distributions throughout the test section and in wall boundary layers were measured and correlated with flight data on typical aircraft boundary layer conditions. Flight conditions are reasonably simulated by the observed airflow, both with and without artificial boundary layer thickening. Author

Author(s):
Eastlake, C. N. ; Ditmer, E. E.
Author Organization(s):
SYSTEMS RESEARCH LABS INC DAYTON OHIO
Descriptive Note:
Final technical rept. Apr-Sep 76,
Pagination:
0110

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
AFAPL-TR-76-103
Contract/Grant Number(s):
F33615-76-C-2095
Task Number(s):
07
Project Number(s):
3048
Monitor Series:
TR-76-103
 Subject Terms
Joint Capability Areas:
JCA_5_Command and Control; JCA_5.3_Planning
Communities of Interest:
Air Platforms
Descriptor(s):
*AIR FLOW, *DUCTS, *BOUNDARY LAYER FLOW, VELOCITY, THICKNESS, DISTRIBUTION, LASERS, FLOW FIELDS, TEST FACILITIES
Field(s)/Group(s):
Aerodynamics, Lasers and Masers, Test Facilities, Equipment and Methods, Fluid Mechanics
Keyword(s):
WUAFAPL30480774, PE62203F
Report Date:
1976 Dec 01