Add to ORKGThe interaction of jets, wakes, and vortices on lifting bodies represents a broad spectrum of aerodynamic flow phenomena. A literature survey is presented of 79 research activities in related aerodynamic situations
Jet exhaust flow effects on aerodynamic characteristics of V/STOL aircraft during transition fligh
Final report; Oct 1976-Dec 1976PDFTech Reporthttp://ntl.bts.gov/lib/47000/47000/47000/FAA-RD-77-23_A...
Surface pressure distributions were obtained with model-scale STOL-OTW configurations using various ...
A procedure has been developed to calculate the effects of blowing two jets over a swept tapered win...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77273/1/AIAA-1992-409-534.pd
Transonic wind tunnel tests to determine wake effect of tip-mounted fan-jet engine on reducing tip v...
The results of two separate theoretical investigations are presented. A program was used which is ca...
Flight tests were conducted to verify the results found in ground base facilities of the effect of s...
Issued as Semiannual status report, and Final report, Project no. E-16-674Final report has title: An...
A brief exploratory flight program was conducted at Ames Research Center to investigate the vortex w...
Propulsion device-induced effects on V/STOL aircraft aerodynamics in hover and transition fligh
The study reported here was initiated by observations of condensation trails that occur behind trans...
Propulsion induced effects encountered by moderate- to high-disk loading STOVL or VSTOL aircraft out...
An exploratory wind-tunnel investigation has been made to determine the lift effects of blowing from...
An analysis of the relative influences of for-ward lift-enhancing surfaces on the overall lift and d...
Jet exhaust flow effects on aerodynamic characteristics of V/STOL aircraft during transition fligh
Final report; Oct 1976-Dec 1976PDFTech Reporthttp://ntl.bts.gov/lib/47000/47000/47000/FAA-RD-77-23_A...
Surface pressure distributions were obtained with model-scale STOL-OTW configurations using various ...
A procedure has been developed to calculate the effects of blowing two jets over a swept tapered win...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77273/1/AIAA-1992-409-534.pd
Transonic wind tunnel tests to determine wake effect of tip-mounted fan-jet engine on reducing tip v...
The results of two separate theoretical investigations are presented. A program was used which is ca...
Flight tests were conducted to verify the results found in ground base facilities of the effect of s...
Issued as Semiannual status report, and Final report, Project no. E-16-674Final report has title: An...
A brief exploratory flight program was conducted at Ames Research Center to investigate the vortex w...
Propulsion device-induced effects on V/STOL aircraft aerodynamics in hover and transition fligh
The study reported here was initiated by observations of condensation trails that occur behind trans...
Propulsion induced effects encountered by moderate- to high-disk loading STOVL or VSTOL aircraft out...
An exploratory wind-tunnel investigation has been made to determine the lift effects of blowing from...
An analysis of the relative influences of for-ward lift-enhancing surfaces on the overall lift and d...
Jet exhaust flow effects on aerodynamic characteristics of V/STOL aircraft during transition fligh
Final report; Oct 1976-Dec 1976PDFTech Reporthttp://ntl.bts.gov/lib/47000/47000/47000/FAA-RD-77-23_A...
Surface pressure distributions were obtained with model-scale STOL-OTW configurations using various ...