Issue
Licensed
Unlicensed
Requires Authentication
Volume 25, Issue 1
Contents
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Requires Authentication UnlicensedCONTENTSLicensedMarch 1, 2008
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Requires Authentication UnlicensedA Method for Reducing Jet Engine Thermal SignatureLicensedMarch 1, 2008
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Requires Authentication UnlicensedEffect of Forward and Aft Lean on the Performance of a Transonic Compressor RotorLicensedMarch 1, 2008
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Requires Authentication UnlicensedExperimental Studies of Low Emission Vortex BurnerLicensedMarch 1, 2008
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Requires Authentication UnlicensedHybrid problems of determining unknown shape of bladings in 3-D compressible steady rotational flow in rotorLicensedMarch 1, 2008
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Requires Authentication UnlicensedBateman's Variational Principle for Turbomachinery AerodynamicsLicensedMarch 1, 2008
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Requires Authentication UnlicensedA Generalized Variational Principle for Inverse Problem of 3-D Unsteady Compressible Flow around Oscillating WingsLicensedMarch 1, 2008
