STOL High-Lift Design Study Volume II. Bibliography

Item

Title
STOL High-Lift Design Study Volume II. Bibliography
Date
1971
Index Abstract
Not Available
Photo Quality
Not Needed
Report Number
AFFDL TR 71-26 Volume II
Creator
May, Fred
Widdison, Coli A.
Corporate Author
Boeing Company
Laboratory
Air Force Flight Dynamics Laboratory
Extent
337
Identifier
AD0724186
Access Rights
This document has been approved for public release and sale; its distribution is unlimited.
Distribution Classification
1
Contract
F33615-70-C-1277
DoD Project
None Given
DoD Task
None Given
DTIC Record Exists
No
Distribution Change Authority Correspondence
None
Distribution Conflict
No
Abstract
The state of the art of STOL aerodynamic technology for selected lift/propulsion concepts has been surveyed to identify the available test data and prediction methods in the literature. The report consists of two volumes. In Volume I important areas of technology and information necessary for the evaluation of STOL aircraft aerodynamics are listed; the aerodynamic test data and prediction methodology relevant to the deflected slipstream and externally blown flap concepts are assessed, with emphasis on the latter; an empirical method for the prediction of the longitudinal aerodynamic characteristics of externally blown flap configurations is presented; and high-lift technology for five lift/propulsion concepts is assessed in application to a medium-sized STOL transport. Volume II consists of a bibliography that resulted from a literature search for aerodynamic information related to seven lift/propulsion concepts suitable for STOL aircraft. The bibliography contains references to approximately 900 reports classified by concept and by technological area.
Report Availability
Full text available
Date Issued
1971-04
Provenance
Bombardier/Aero
Type
report
Format
1 online resource