Flow Separation Delay on NACA 4415 Airfoil Using Plasma Actuator Effect.
- Published in:
- International Review of Aerospace Engineering, 2019, v. 12, n. 4, p. 180, doi. 10.15866/irease.v12i4.16219
- By:
- Publication type:
- Article
Works matching IS 19737459 AND DT 2019 AND VI 12 AND IP 4
Results: 5
1
2
Characteristics of Potential Sources - Vertical Force, Torque and Current on Penetration Depth for Quality Assessment in Friction Stir Welding of AA 6061 Pipes.
- Published in:
- International Review of Aerospace Engineering, 2019, v. 12, n. 4, p. 195, doi. 10.15866/irease.v12i4.16362
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- Publication type:
- Article
3
New Reactive Space Engine.
- Published in:
- International Review of Aerospace Engineering, 2019, v. 12, n. 4, p. 171, doi. 10.15866/irease.v12i4.16125
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- Publication type:
- Article
4
The Impact Force Acting on a Normal Flat Plate Due to Non-Continuum Flow Issuing from Planner Exit with Different Speed Ratio.
- Published in:
- International Review of Aerospace Engineering, 2019, v. 12, n. 4, p. 187, doi. 10.15866/irease.v12i4.15171
- By:
- Publication type:
- Article
5
Optimization Techniques for Prognostics of On-Board Electromechanical Servomechanisms Affected by Progressive Faults.
- Published in:
- International Review of Aerospace Engineering, 2019, v. 12, n. 4, p. 160, doi. 10.15866/irease.v12i4.17356
- By:
- Publication type:
- Article