A methodology for determination of baseline specifications of a non-rigid airship

AIAA's 3rd Annual Aviation Technology, Integration, and Operations (ATIO) Forum

Volumn , Issue , 2003, Pages

  Pant, Rajkumar S ^a  

^a INDIAN INSTITUTE OF TECHNOLOGY BOMBAY   (India)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 84894481594     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (10)

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3. Young, A.D. The calculations of the total and skin friction drags of bodies of revolution at zero incidence. ARC R&M, 1874, London, HMSO, 1939.
4. Hoerner, S.F. Fluid Dynamic Drag. New Jersey, Published by the author, (Midland Park), (1957).
5. Raymer D. P., Aircraft Design: A Conceptual Approach, AIAA Education series, AIAA, Washington D.C., USA, 1989.
6. Stinton D., The Design of The Aeroplane, Blackwell Science Limited, UK, ISBN 0 632 01 877 1, 1995.
7. Netherclift, O. J., Airships Today and Tomorrow, Publication No. 4., The Airship Association Ltd., UK, 1993
8. th November 1986.
9. Anonymous, US-LTA 185M airship specifications, Revision A, Pvt. Communication, US-LTA Corp., Oregon, US
10. Jane's All the World's aircraft, LTA Section, Jane's Information Group, Surrey, UK, 1999-2000