Results 201 to 210 of about 798 (239)
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Numerical and Experimental Investigations of Fluidic Thrust Vectoring Mechanism

International Journal of Aerospace Innovations, 2012
The objective of this paper is to investigate the fluidic thrust vectoring (FTV) effects of a secondary jet on the primary flow in a converging-diverging nozzle. The experiments are performed with a nozzle pressure ratio (NPR) of 4-10, a secondary pressure ratio (SPR) of 1 or 2, and two different secondary jet locations.
Li Li, Tsutomu Saito
openaire   +1 more source

A Survey of Fluidic Thrust Vectoring Nozzle by Numerical Analysis

Applied Mechanics and Materials, 2013
Numerical investigations are conducted to simulate the flow field of a 2D converging-diverging nozzle, for fluidic thrust vectoring. The numerical simulation of nozzle flow is carried out with Navier-Stokes equations model. Simulations are done with different primary and secondary jet conditions.
Li Li, Zhi Hui Shi, Tsutomu Saito
openaire   +1 more source

Multi-axis fluidic thrust vectoring of supersonic jets via counterflow

35th Aerospace Sciences Meeting and Exhibit, 1997
The most common techniques currently used to efficiently vector supersonic jets require external flaps and or pivoting devices. Fluidic thrust vectoring using counterflow eliminates the need for such complex hardware. Thus, the promise of decreases in both weight and drag as well as increased maneuverability makes this technique an attractive ...
F. Alvi   +7 more
openaire   +1 more source

Fluidic scale model multi-plane thrust vector control test results

29th Joint Propulsion Conference and Exhibit, 1993
An experimental investigation has been conducted at the NASA Langley 16-Foot Transonic Tunnel Static Test Facility to determine the concept feasibility of using fluidics to achieve multiplane thrust vector control in a 2D convergent-divergent (2D-CD) fixed aperture nozzle.
CHARLES CHIARELLI   +3 more
openaire   +1 more source

Fluidic Thrust Vector Control of Supersonic Jet Using Coflow Injection

Journal of Propulsion and Power, 2012
The purpose of this research is to investigate the operation condition of fluidic thrust vector using injection of the control flow tangential to the main jet direction; co-flow injection. The physical model of concern includes a chamber and a supersonic nozzle for supersonic main jet injection, and two chambers with slots for control flow injection ...
Hong-Gye Sung, Jun-Young Heo
openaire   +1 more source

Performance Analysis of Fluidic Thrust Vector Control System

The Proceedings of Conference of Chugoku-Shikoku Branch, 2021
Yoichiro Takahashi, Yuichi Maruyama
openaire   +1 more source

A System Study On Fluidic Thrust Vectoring

20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015
Hilbert V. Pelt   +2 more
openaire   +1 more source

Performance Studies of Shock Vector Control Fluidic Thrust Vectoring

43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2007
Andrew Neely, Fernando Gesto, John Young
openaire   +1 more source

Integrative oncology: Addressing the global challenges of cancer prevention and treatment

Ca-A Cancer Journal for Clinicians, 2022
Jun J Mao,, Msce   +2 more
exaly  

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