Demonstration of fluidic throat skewing for thrust vectoring in structurally fixed nozzles

Journal of Engineering for Gas Turbines and Power

Volumn 123, Issue 3, 2001, Pages 502-507

  Yagle, P J ^a   Miller, D N ^a   Ginn, K B ^a   Hamstra, J W ^a  

^a Lockheed Marlin Aeronautics Company   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FLUIDIC THROAT SKEWING;

DISCHARGE (FLUID MECHANICS); EXPANSION; NOZZLES; PLANERS; VECTORS;

GAS TURBINES;

AIRCRAFT; DESIGN; FLOW CONTROL; FLUIDICS;

EID: 0035391010     PISSN: 07424795     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1361109     Document Type: Article

References (13)

1. Fluidic throat skewing for thrust vectoring in fixed geometry nozzles
2. Conceptual development of fixed-geometry nozzles using fluidic injection for throat-area control
3. Extending flow control of fixed nozzles through systematic design: Introducing assisted reinjection
4. Inlet and nozzle tech. for 21st century aircraft
5. Fluidic scale model multi-plane thrust vector control test results
6. Thrust vector control of rectangular jets using counter flow
7. Lessons learned in the development of a national program
8. Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional C-D nozzle
9. A static investigation of fixed-geometry nozzles using fluidic injection for throat-area control
10. A diagonally inverted LU implicit multigrid scheme
11. The k-kl turbulence model and wall layer model for compressible flows
12. Static investigation of a multiaxis thrust-vectoring nozzle With variable internal contouring ability