Add to ORKGExperimental Studies Were Carried Out With Ejectors Having 2D And Multi Jet Nozzles To Determine If They Could Be Adopted To Drive A Low Speed Tunnel .A Model Tunnel Was Constructed And Results Obtained From Different Ejector Configurations Have Been Compared.\ud \ud The Study Suggests That An Annular Ejector Is Promising As A Candidate Configuration For Further Work Leading To An Application As A Wind Tunnel Drive
A fundamental exploratory experiment is conducted assessing the performance of a one-sided ejector w...
Wind tunnel model tests were conducted to demonstrate the aerodynamic performance improvements of a ...
Due to the large disturbance created by the sonic boom, supersonic flight is strictly controlled by ...
Experimental studies were carried out with ejectors having 2D\ud and multijet nozzles to determine i...
Some preliminary experiments were carried out in a small (0.1x0.25 metre) tunnel to study the feasib...
This Report Gives The Results Of The Tests Conducted For CRE\ud (Aircraft) Directorate Of Aeronautic...
In This Study, The Usefulness Of Secondary Air Jets (Located In Front Of The Ejection Seat) In Reduc...
In This Study, The Usefulness Of Secondary Air Jets (Located In Front Of The Ejection Seat) In Reduc...
The contribution deals with the development of design of new conception of ejector with twelve prima...
The article deals with experimental and numerical investigation of an air to air supersonic ejector ...
Cover title."June 1962."Fluid mechanics; Research and development facilities.Includes bibliographica...
The results of an experimental investigation to determine the feasibility of conducting engine/exter...
Four ejectors mounted in each pod under each wing and powered with compressed air were used to simul...
The wind tunnel is the most fundamental test equipment for aircraft testing and studying aerodynamic...
A technique is developed for determining a representative value of the maximum efficiency that can b...
A fundamental exploratory experiment is conducted assessing the performance of a one-sided ejector w...
Wind tunnel model tests were conducted to demonstrate the aerodynamic performance improvements of a ...
Due to the large disturbance created by the sonic boom, supersonic flight is strictly controlled by ...
Experimental studies were carried out with ejectors having 2D\ud and multijet nozzles to determine i...
Some preliminary experiments were carried out in a small (0.1x0.25 metre) tunnel to study the feasib...
This Report Gives The Results Of The Tests Conducted For CRE\ud (Aircraft) Directorate Of Aeronautic...
In This Study, The Usefulness Of Secondary Air Jets (Located In Front Of The Ejection Seat) In Reduc...
In This Study, The Usefulness Of Secondary Air Jets (Located In Front Of The Ejection Seat) In Reduc...
The contribution deals with the development of design of new conception of ejector with twelve prima...
The article deals with experimental and numerical investigation of an air to air supersonic ejector ...
Cover title."June 1962."Fluid mechanics; Research and development facilities.Includes bibliographica...
The results of an experimental investigation to determine the feasibility of conducting engine/exter...
Four ejectors mounted in each pod under each wing and powered with compressed air were used to simul...
The wind tunnel is the most fundamental test equipment for aircraft testing and studying aerodynamic...
A technique is developed for determining a representative value of the maximum efficiency that can b...
A fundamental exploratory experiment is conducted assessing the performance of a one-sided ejector w...
Wind tunnel model tests were conducted to demonstrate the aerodynamic performance improvements of a ...
Due to the large disturbance created by the sonic boom, supersonic flight is strictly controlled by ...