Works matching IS 17572258 AND DT 2012 AND VI 4 AND IP 3/4
Results: 6
Dynamic Landing Response Analysis of a Flexible Tailless Delta Wing Aircraft.
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- International Journal of Aerospace Innovations, 2012, v. 4, n. 3/4, p. 103, doi. 10.1260/1757-2258.4.3-4.103
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- Article
Modeling and Simulation of Wake Encounter for a Fighter Aircraft.
- Published in:
- International Journal of Aerospace Innovations, 2012, v. 4, n. 3/4, p. 65, doi. 10.1260/1757-2258.4.3-4.65
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- Article
A High-Speed Towing Tank for Hydrodynamics and Cavitation Experiments.
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- International Journal of Aerospace Innovations, 2012, v. 4, n. 3/4, p. 85, doi. 10.1260/1757-2258.4.3-4.85
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- Article
Smoke Flow Visualizations for the Study of Surface Dielectric Barrier Discharge Induced Flow Field.
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- International Journal of Aerospace Innovations, 2012, v. 4, n. 3/4, p. 75, doi. 10.1260/1757-2258.4.3-4.75
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- Article
Human Response Characteristics to Impact Conditions During Spacecraft Takeoff and Impact Landing.
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- International Journal of Aerospace Innovations, 2012, v. 4, n. 3/4, p. 95, doi. 10.1260/1757-2258.4.3-4.95
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- Article
Development, Uniformity and Peak Heating of a Hypersonic Laminar Near-Wake Flow.
- Published in:
- International Journal of Aerospace Innovations, 2012, v. 4, n. 3/4, p. 119, doi. 10.1260/1757-2258.4.3-4.119
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- Article