NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
A vectored-engine-over-wing propulsive-lift conceptAn experimental investigation has been conducted to evaluate a unique engine-over-wing propulsive-life scheme for providing maneuver improvement in the subsonic-transonic speed regime. The concept combines the benefits of vectored thrust for added circulation and spanwise blowing for leading-edge-vortex augmentation so as to provide full angle-of-attack aerodynamic improvements. Results of a series of wind tunnel tests employing a powered research model illustrate the propulsive/aerodynamic features of the concept.
Document ID
19760087419
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bradley, R. G. (General Dynamics Corp. Aerospace Technology Dept., Fort Worth, Tex., United States)
Jeffries, R. R. (USAF, Flight Dynamics Laboratory, Wright-Patterson AFB Ohio, United States)
Capone, F. J. (NASA Langley Research Center Propulsion Integration Section, Hampton, Va., United States)
Date Acquired
August 8, 2013
Publication Date
September 1, 1976
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 76-917
Report Number: AIAA PAPER 76-917
Accession Number
76A47684
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