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