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A hybrid airship concept for Naval missionsA preliminary analysis of a hybrid semibuoyant delta-planform airship was performed using a computer synthesis program. The delta-planform hull shape was studied parametrically to determine the effects on vehicle performance for two Navy antisubmarine missions. The effects of buoyancy ratio, design speed, and altitude were also studied. The results suggest that long-range mission vehicles require a near buoyant or fully buoyant design and that there is no special advantage to the use of a lifting-body hull shape. For shorter-range missions, hybrid vehicles may have merit, and optimum vehicle buoyancy varies depending on whether a minimum-weight or minimum-fuel-consumption design is desired. As compared with conventionally shaped airships, the benefits, if any, from a lifting-body configuration will be limited to missions requiring relatively higher flight speeds.
Document ID
19760062434
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Harper, M.
(NASA Ames Research Center Moffett Field, Calif., United States)
Date Acquired
August 8, 2013
Publication Date
September 1, 1976
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 76-923
Accession Number
76A45400
Distribution Limits
Public
Copyright
Other

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