Mathcad Model For The Estimation Of Cost And Main Characteristics Of Air Cushion Vehicles In The Preliminary Design Stage PDF Download

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MathCAD Model for the Estimation of Cost and Main Characteristics of Air-cushion Vehicles in the Preliminary Design Stage

MathCAD Model for the Estimation of Cost and Main Characteristics of Air-cushion Vehicles in the Preliminary Design Stage
Author: Georgios Gougoulidis
Publisher:
Total Pages: 100
Release: 2005
Genre:
ISBN:

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(Cont.) For the validation of the code, LCAC (Landing Craft Air Cushion) is used as the reference vehicle. The values of LCAC design parameters that are known, are input in the code and crosschecked with the outputs. Iterative procedures have been applied to the code in order to correct the trend lines according to the reference model. The development of this MathCAD model is directly related to the lack of software dealing with the design of ACVs in the market. Conventional ship design tools are widespread and used even by students. On the other hand, ACV design programs are possessed by the companies that design this kind of crafts and are not widely available. In the following pages, together with the analysis of the model developed, the associated theory is presented so that the reader has a complete image of what an ACV is and how it works. Hence, this thesis is not a manual of a program, but a combination of theory and application intended to help the reader-user understand the design process of ACVs.


A Study of Requirements, Model Configurations, and Test Plans for Air Cushion System Comparison Tests

A Study of Requirements, Model Configurations, and Test Plans for Air Cushion System Comparison Tests
Author: J. Ryken
Publisher:
Total Pages: 40
Release: 1979
Genre:
ISBN:

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The Navy plans to test several models of air cushion vehicles with different cushion systems. A set of model design requirements suitable for all the models was developed by the Navy with the assistance of Bell Aerospace Textron and other contractors. The proposed DTNSRDC Model Test Program was reviewed. Minor changes and additions were suggested. A preliminary model configuration using Bell cushion philosophy was proposed. Ranges of bag and cushion pressures and airflows were established for the model. Two existing model fans from an existing model of the AALC JEFF(B) could provide the required nominal flow and pressure. Bell recommends installing four of these existing fans to permit testing over a wide range of flows. Cost and schedule estimates for the model detail design and construction were prepared. The schedule is shown in this report; cost estimates were provided under separate cover. (Author).