A comprehensive numerical model investigating the thermal-dynamic performance of scientific balloon

Abstract The increase of balloon applications makes it necessary for a comprehensive understanding of the thermal and dynamic performance of scientific balloons. This paper proposed a novel numerical model to investigate the thermal and dynamic characteristics of scientific balloon in both ascending and floating conditions. The novel model consists of a dynamic model and thermal model, the dynamic model was solved numerically by a computer program developed with Matlab/Simulink to calculate the velocity and trajectory, the thermal model was solved by the Fluent program to find out the balloon film temperature distribution and inner Helium gas velocity and temperature field. These models were verified by comparing the numerical results with experimental data. Then the thermal and dynamic behavior of a scientific balloon in a real environment were simulated and discussed in details.

[1]  Steady state model for the thermal regimes of shells of airships and hot air balloons , 1992 .

[2]  C. Yang,et al.  A comprehensive numerical model examining the thermal performance of airships , 2011 .

[3]  Baoyin Song,et al.  Thermal Performance of Stratospheric Airships During Ascent and Descent , 2009 .

[4]  S. Patankar Numerical Heat Transfer and Fluid Flow , 2018, Lecture Notes in Mechanical Engineering.

[5]  Xiaojian Li,et al.  Performance simulation of high altitude scientific balloons , 2012 .

[6]  L. Ruan,et al.  Transient thermal behavior of stratospheric balloons at float conditions , 2010 .

[7]  H. M. Cathey,et al.  The NASA super pressure balloon – A path to flight , 2009 .

[8]  Anthony Colozza,et al.  Initial Feasibility Assessment of a High Altitude Long Endurance Airship , 2013 .

[9]  L. Morris,et al.  Scientific Ballooning Handbook , 1975 .

[10]  Rodger E. Farley,et al.  Balloon Ascent: 3-D Simulation Tool for the Ascent and Float of High-Altitude Balloons , 2005 .

[11]  H. M. Cathey,et al.  Thermal performance modeling of NASA’s scientific balloons , 2002 .

[12]  K. Harada,et al.  Experimental study of thermal modeling for stratospheric platform airships , 2003 .

[13]  F. Kreith,et al.  Numerical Prediction of the Performance of High Altitude Balloons , 1974 .

[14]  Frank P. Incropera,et al.  Fundamentals of Heat and Mass Transfer , 1981 .

[15]  K. Stefan Thermal effects on a high altitude airship , 1983 .

[16]  L. Carlson,et al.  New thermal and trajectory model for high-altitude balloons , 1981 .