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Computer Programs for Calculating and Plotting the Stability Characteristics of a Balloon Tethered in a WindComputer programs for calculating the stability characteristics of a balloon tethered in a steady wind are presented. Equilibrium conditions, characteristic roots, and modal ratios are calculated for a range of discrete values of velocity for a fixed tether-line length. Separate programs are used: (1) to calculate longitudinal stability characteristics, (2) to calculate lateral stability characteristics, (3) to plot the characteristic roots versus velocity, (4) to plot the characteristic roots in root-locus form, (5) to plot the longitudinal modes of motion, and (6) to plot the lateral modes for motion. The basic equations, program listings, and the input and output data for sample cases are presented, with a brief discussion of the overall operation and limitations. The programs are based on a linearized, stability-derivative type of analysis, including balloon aerodynamics, apparent mass, buoyancy effects, and static forces which result from the tether line.
Document ID
19730023220
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Bennett, R. M.
(NASA Langley Research Center Hampton, VA, United States)
Bland, S. R.
(NASA Langley Research Center Hampton, VA, United States)
Redd, L. T.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1973
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-2740
L-8542
Report Number: NASA-TM-X-2740
Report Number: L-8542
Accession Number
73N31952
Funding Number(s)
PROJECT: RTOP 501-22-04-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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