NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Aerodynamic design of electric and hybrid vehicles: A guidebookA typical present-day subcompact electric hybrid vehicle (EHV), operating on an SAE J227a D driving cycle, consumes up to 35% of its road energy requirement overcoming aerodynamic resistance. The application of an integrated system design approach, where drag reduction is an important design parameter, can increase the cycle range by more than 15%. This guidebook highlights a logic strategy for including aerodynamic drag reduction in the design of electric and hybrid vehicles to the degree appropriate to the mission requirements. Backup information and procedures are included in order to implement the strategy. Elements of the procedure are based on extensive wind tunnel tests involving generic subscale models and full-scale prototype EHVs. The user need not have any previous aerodynamic background. By necessity, the procedure utilizes many generic approximations and assumptions resulting in various levels of uncertainty. Dealing with these uncertainties, however, is a key feature of the strategy.
Document ID
19810004432
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kurtz, D. W.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 4, 2013
Publication Date
September 30, 1980
Subject Category
Urban Technology And Transportation
Report/Patent Number
NASA-CR-163744
JPL-PUB-80-69
Report Number: NASA-CR-163744
Report Number: JPL-PUB-80-69
Accession Number
81N12943
Funding Number(s)
CONTRACT_GRANT: DE-AI01-78CS-54209
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available