Titlebook: Recent Advances in the Aerospace Sciences; In Honor of Luigi Cr Corrado Casci (Chairman),Claudio Bruno Book 1985 Plenum Press, New York 198

PACK

The Relationship between Temperature and Velocity in Turbulent Boundary Layers with Injectionneering papers by Crocco on the corresponding results in laminar flow. As a result a number of authors have derived a simple algebraic form for the relation, the Crocco relation. This simple form has been found to be in close agreement with experimental results over a wide range of conditions althou

genesis

排他

Linear Model of Convective Heat Transfer in a Spray linear analysis of gas-phase unsteadiness and transient heating of the droplets..One-dimensional, unsteady solutions for the gas temperature and droplet temperature are obtained. In addition to the general solution, asymptotic solutions for large liquid thermal inertia and small liquid thermal iner

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DEBT

支架

Theory of Idealized Coal Devolatilizationsolid-phase species, which thermally decompose to yield a single gas-phase species. Devolatilization is described by a classical linear theory involving both equilibrium and kinetic characteristics of each solid-phase species. The temperature history of the particle is treated in two different ways

茁壯成長(zhǎng)

Model of Low-Reynolds-Number Wall Turbulence for Equilibrium Layersve agreement with that described by Shubauer. The same initial conditions have been assumed for the whole range of favorable and adverse pressure gradients considered. The free-stream pressure gradient influences the mean quantities and the turbulence-energy balance in a manner that is in agreement with experiment.

Hippocampus

Linear Model of Convective Heat Transfer in a Sprayolutions are piecewise analytic and a domain of independence of boundary values is obtained. In general, two characteristic times (and their associated space scales) appear in the solutions, namely a gas residence time and a droplet heating time.

kindred

Minimax Optimal Control and Its Application to the Reentry of a Space Gliderte..Numerical results are obtained by means of the sequential gradient-restoration algorithm for solving optimal control problems on a digital computer. Reference is made to the hypervelocity regime, an exponential atmosphere, and a space glider whose trajectory is controlled by means of the angle of attack and the angle of bank.

恃強(qiáng)凌弱的人

The Relationship between Temperature and Velocity in Turbulent Boundary Layers with Injectiontend some of the derivations to boundary-layer flows over porous surfaces and the results are found to be in good agreement with experiment, even in highly nonequilibrium layers, for example, in the boundary layer downstream of a porous surface.