Question 9 of 13: Rate of Rise of a Hydrogen Balloon (Drag Chart)
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
04-BS-7 Mechanics of Fluids — National Examination, 2013-May. Three (3) hours duration, closed book. Section A (Calculative, 9 questions, do 7) and Section B (Analytical, 4 questions, do 3); every question is answered below regardless of the exam's "do N of M" instruction, so the set is a complete study resource.
Reference texts: Crowe, C.T., Elger, D.F. & Roberson, J.A., Engineering Fluid Mechanics (the exam's own Moody chart and drag-coefficient chart are reproduced from this text); Douglas, J.F., Gasiorek, J.M., Swaffield, J.A. & Jack, L.B., Fluid Mechanics; White, F.M., Fluid Mechanics.
Check — assumptions used across this paper:
Where a question does not restate an ambient temperature, air is taken at the ISA sea-level standard of 15°C, giving ρair = 1.21 kg/m³ (the Constants table's 15°C value) — used in Q5, Q6, Q7 and Q9.
Q8's Moody chart and Q9's sphere drag-coefficient chart are supplied as attachments. Both are solved via the equations the charts themselves plot: the Colebrook–White equation for Q8 (the Moody chart is a graphical solution of Colebrook–White) and the Morrison (2013) curve-fit for sphere drag versus Reynolds number for Q9 (which reproduces the published "Sphere" curve to within a few percent over this Re range).
Q1, Q3 and Q11 depend on their figures; the relevant crop of the exam page is reproduced beside each, and every reading used is taken from it.
Question 9: Rate of Rise of a Hydrogen Balloon (Drag Chart) (5 marks)
At terminal (constant) rise velocity, net buoyant force equals drag.
Find. Terminal (constant) rate of rise through the atmosphere.
Approach. Compute the net buoyant force (air displaced minus hydrogen contained, structure mass negligible), then solve iteratively for the velocity at which sphere drag (from the standard sphere drag-coefficient curve versus Reynolds number) balances that force.
Check: Cd(Re) is obtained from the Morrison (2013) curve-fit, which reproduces the published sphere-drag curve (the same one reprinted in the attachment) to within a few percent over the relevant Reynolds-number range.
Balloon volume and area. $V=\pi D^3/6=\pi(0.6)^3/6=0.1131\ \text{m}^3$; $A=\pi D^2/4=\pi(0.6)^2/4=0.2827\ \text{m}^2$.
Hydrogen density (ideal gas). $\rho_{H_2}=\dfrac{P}{R_{H_2}T}=\dfrac{100{,}000}{4120\times288.15}=0.0842\ \text{kg/m}^3$.
Net buoyant force. Structure mass negligible, so
$$F_{net} = (\rho_{air}-\rho_{H_2})Vg = (1.21-0.0842)\times0.1131\times9.81 = 1.249\ \text{N}$$
Terminal velocity from drag balance. Solving $F_{net}=C_D(Re)\,\tfrac12\rho_{air}V_t^2A$ iteratively (Cd from the sphere drag curve) converges at
$$Re = \frac{V_tD}{\nu_{air}} \approx 1.65\times10^5,\qquad C_D\approx0.434$$
$$\boxed{V_t \approx 4.10\ \text{m/s}}$$