NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Wing aerodynamic loading caused by jet-induced lift associated with STOL-OTW configurationsSurface pressure distributions were obtained with model-scale STOL-OTW configurations using various nozzles designed to promote flow attachment to the wing-flap surface. The nozzle configurations included slot-types and both circular and slot nozzles with external flow deflectors. The wing aerodynamic loading caused by the jet-induced lift is presented in conventional terms of delta p/q as a function of chordwise surface distance in the nozzle centerline plane as well as outboard of the nozzle centerline. Included in the geometric variables affecting the wing loading are nozzle roof/deflector angle, chordwise location of the nozzle, wing size, and flap deflection angle.
Document ID
19790063333
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Von Glahn, U. (NASA Lewis Research Center Cleveland, OH, United States)
Groesbeck, D. (NASA Lewis Research Center Cleveland, Ohio, United States)
Date Acquired
August 9, 2013
Publication Date
August 1, 1979
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 79-1664
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Atmospheric Flight Mechanics Conference
Location: Boulder, CO
Start Date: August 6, 1979
End Date: August 8, 1979
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
79A47346
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.

Related Records

There are no records associated with this record.
No Preview Available