The basic aerodynamics of floatation

Journal Article · Thu Sep 01 00:00:00 EDT 1983 · J. Fluids Eng.; (United States)

DOI:https://doi.org/10.1115/1.3240998· OSTI ID:6702332

Davies, M J; Wood, D H

The original derivation of the basic theory governing the aerodynamics of both hovercraft and modern floatation ovens, requires the validity of some extremely crude assumptions. However, the basic theory is surprisingly accurate. It is shown that this accuracy occurs because the final expression of the basic theory can be derived by approximating the full Navier-Stokes equations in a manner that clearly shows the limitations of the theory. These limitations are used in discussing the relatively small discrepancies between the theory and experiment, which may not be significant for practical purposes.

• Research Organization: John Lysaght (Aust.) Ltd., Port Kembia
• OSTI ID: 6702332
• Journal Information: J. Fluids Eng.; (United States), Vol. 105:3
• Country of Publication: United States
• Language: English

Related Subjects

37 INORGANIC
ORGANIC
PHYSICAL AND ANALYTICAL CHEMISTRY
FLOTATION
AERODYNAMICS
NAVIER-STOKES EQUATIONS
ACCURACY
AIR CUSHION VEHICLES
OVENS
APPLIANCES
DIFFERENTIAL EQUATIONS
EQUATIONS
FLUID MECHANICS
MECHANICS
PARTIAL DIFFERENTIAL EQUATIONS
SEPARATION PROCESSES
VEHICLES
400105* - Separation Procedures