Theory

Gas Well Deliverability

Overview

Gas well performance differs fundamentally from oil wells due to:

  • High flow velocities โ€” Gas compressibility creates turbulence near wellbore
  • Pressure-dependent properties โ€” ฮผg, ฯg, Z vary significantly with pressure
  • Non-Darcy flow โ€” Inertial/turbulent effects at high rates
  • Pseudo-pressure โ€” Required for rigorous gas flow analysis

Gas well deliverability analysis determines:

  • AOF (Absolute Open Flow) โ€” Maximum theoretical rate
  • Productivity โ€” Relationship between rate and pressure drawdown
  • Backpressure curve โ€” Rate vs. (pยฒ) or pseudo-pressure relationship
  • Completion efficiency โ€” Skin effects and damage quantification

Darcy vs. Non-Darcy Flow

Darcy Flow (Laminar)

At low velocities, gas flow follows Darcy's law (linear relationship):

qsc=khฮผgBg2ฯ€lnโก(re/rw)โˆ’0.75+s(pRโˆ’pwf)q_{sc} = \frac{k h}{\mu_g B_g} \frac{2\pi}{\ln(r_e/r_w) - 0.75 + s} (p_R - p_{wf})

Or in pseudo-steady state using real gas pseudo-pressure:

qsc=kh1424Tm(pR)โˆ’m(pwf)lnโก(re/rw)โˆ’0.75+sq_{sc} = \frac{k h}{1424 T} \frac{m(p_R) - m(p_{wf})}{\ln(r_e/r_w) - 0.75 + s}

Where real gas pseudo-pressure is:

m(p)=2โˆซ0ppฮผgZdpm(p) = 2\int_0^p \frac{p}{\mu_g Z} dp

Applicability: Low rate wells, high permeability, large wellbore radius.

Non-Darcy Flow (Turbulent)

At high velocities, inertial (turbulent) effects become significant. The Forchheimer equation adds a rate-squared term:

โˆ’dpdr=ฮผgqkh+ฯgฮฒq2-\frac{dp}{dr} = \frac{\mu_g q}{kh} + \rho_g \beta q^2

Where:

  • ฮฒ\beta = turbulence factor (or inertial resistance coefficient), ftโปยน
  • Second term represents non-Darcy (turbulence) pressure drop

This leads to the backpressure equation:

pR2โˆ’pwf2=aqsc+bqsc2p_R^2 - p_{wf}^2 = a q_{sc} + b q_{sc}^2

Or:

m(pR)โˆ’m(pwf)=aโ€ฒqsc+bโ€ฒqsc2m(p_R) - m(p_{wf}) = a' q_{sc} + b' q_{sc}^2

Physical interpretation:

  • aa term: Darcy (laminar) flow
  • bb term: Non-Darcy (turbulent) flow
  • At high rates, turbulence dominates (b term >> a term)

Non-Darcy Coefficient (D)

The non-Darcy flow coefficient quantifies turbulence:

D=ba=Fkhฮฒ1424TD = \frac{b}{a} = \frac{F k h \beta}{1424 T}

Where:

  • FF = turbulence factor (dimensionless, typically 1-100)
  • Higher D โ†’ More turbulence, steeper backpressure curve

Typical D values:

  • Low perm tight gas (0.1 md): D = 0.001 to 0.01
  • Moderate perm (1 md): D = 0.0001 to 0.001
  • High perm (100 md): D = 0.00001 to 0.0001

Estimating D (Jones-Blount-Glaze Correlation)

D=3.161ร—10โˆ’12ฮฒฮณgTkhrw2ฮผgD = 3.161 \times 10^{-12} \frac{\beta \gamma_g T}{k h r_w^2 \mu_g}

Where ฮฒ\beta (turbulence factor) can be estimated from:

ฮฒ=1.88ร—1010k1.2\beta = \frac{1.88 \times 10^{10}}{k^{1.2}}

Data needed: k, h, rw, T, ฮณg, ฮผg (all at average reservoir conditions).


Backpressure Testing

Four-Point Test Procedure

  1. Shut in well โ†’ measure pR (stabilized)
  2. Flow at rate qโ‚ โ†’ measure pwf,1 (stabilized)
  3. Flow at rate qโ‚‚ โ†’ measure pwf,2 (stabilized)
  4. Flow at rate qโ‚ƒ โ†’ measure pwf,3 (stabilized)
  5. Flow at rate qโ‚„ โ†’ measure pwf,4 (stabilized)

Calculating a, b (or n)

Plot (pR2โˆ’pwf2)(p_R^2 - p_{wf}^2) vs. qscq_{sc} on log-log paper.

Slope = n (deliverability exponent):

  • n = 1.0 โ†’ Pure Darcy flow (no turbulence)
  • n = 0.5 โ†’ Fully turbulent flow
  • n = 0.6 to 0.8 โ†’ Typical gas wells

Backpressure equation:

qsc=C(pR2โˆ’pwf2)nq_{sc} = C (p_R^2 - p_{wf}^2)^n

Or modern form:

pR2โˆ’pwf2=aqsc+bqsc2p_R^2 - p_{wf}^2 = a q_{sc} + b q_{sc}^2

Absolute Open Flow (AOF):

qAOF=C(pR2)n=CpR2nq_{AOF} = C (p_R^2)^n = C p_R^{2n}

Pseudo-Steady State Gas Flow

For bounded reservoirs (closed drainage volume), use pseudo-steady state equations.

PSS Darcy Flow

qsc=kgh[m(pR)โˆ’m(pwf)]1424T[lnโก(re/rw)โˆ’0.75+s]q_{sc} = \frac{k_g h [m(p_R) - m(p_{wf})]}{1424 T [\ln(r_e/r_w) - 0.75 + s]}

Where:

  • rer_e = external drainage radius, ft
  • rwr_w = wellbore radius, ft
  • ss = skin factor (dimensionless)

PSS Non-Darcy Flow

m(pR)โˆ’m(pwf)=1424Tqsckgh[lnโก(re/rw)โˆ’0.75+s]+Dqscm(p_R) - m(p_{wf}) = \frac{1424 T q_{sc}}{k_g h} [\ln(r_e/r_w) - 0.75 + s] + D q_{sc}

Combining:

m(pR)โˆ’m(pwf)=aqsc+Dqsc2m(p_R) - m(p_{wf}) = a q_{sc} + D q_{sc}^2

Where:

a=1424Tkgh[lnโก(re/rw)โˆ’0.75+s]a = \frac{1424 T}{k_g h} [\ln(r_e/r_w) - 0.75 + s]

Time to Pseudo-Steady State

Before PSS is reached, gas wells exhibit transient flow. Time to reach PSS:

For Gas (Low Compressibility Liquid)

tPSS=380ฯ•ฮผgctre2kt_{PSS} = \frac{380 \phi \mu_g c_t r_e^2}{k}

Where:

  • tPSSt_{PSS} = time to PSS, hours
  • ฯ•\phi = porosity, fraction
  • ฮผg\mu_g = gas viscosity, cP
  • ctc_t = total compressibility, psiโปยน
  • rer_e = drainage radius, ft
  • kk = permeability, md

Typical values:

  • High perm (100 md), small drainage (500 ft): tPSS โ‰ˆ 5 hours
  • Low perm (0.1 md), large drainage (2000 ft): tPSS โ‰ˆ 2000 hours

Skin Factor and Wellbore Effects

Total Skin Factor

stotal=sdamage+sperforation+spartialโ€‰penetration+sdeviation+sturbulences_{total} = s_{damage} + s_{perforation} + s_{partial\,penetration} + s_{deviation} + s_{turbulence}

Components:

  • sdamages_{damage}: Formation damage near wellbore
  • sperforations_{perforation}: Perforation geometry and density
  • spartialpenetrations_{partial penetration}: Limited perforated interval
  • sdeviations_{deviation}: Deviated well effects
  • sturbulences_{turbulence}: High-velocity non-Darcy effects

Effective Wellbore Radius

Positive skin reduces effective wellbore radius:

rwโ€ฒ=rweโˆ’sr_w' = r_w e^{-s}

Where:

  • rwโ€ฒr_w' = effective wellbore radius, ft
  • rwr_w = actual wellbore radius, ft
  • ss = skin factor

Example:

  • rw = 0.5 ft, s = +5 โ†’ rw' = 0.0034 ft (147ร— reduction!)
  • rw = 0.5 ft, s = -3 โ†’ rw' = 10.0 ft (20ร— increase from stimulation)

Equivalent Skin for Fractures

Hydraulically fractured wells can be represented by equivalent negative skin:

sfrac=lnโก(rwxf/2)s_{frac} = \ln\left(\frac{r_w}{x_f/2}\right)

Where:

  • xfx_f = fracture half-length, ft

Example: xf = 200 ft, rw = 0.5 ft โ†’ sfrac = -6 (excellent stimulation).


Drainage Radius Calculations

For circular drainage area:

re=Aฯ€r_e = \sqrt{\frac{A}{\pi}}

Where AA = drainage area, ftยฒ

Common well spacings:

  • 160 acres: re โ‰ˆ 1490 ft
  • 80 acres: re โ‰ˆ 1053 ft
  • 40 acres: re โ‰ˆ 745 ft

Functions Covered

The following functions implement gas well deliverability calculations. See each function page for detailed parameter definitions, Excel syntax, and usage examples.

FunctionDescriptionUnits
GasFlowRatePSSPSS Darcy gas flow (linear, no turbulence)Mscf/d
GasFlowRatePSSNonDarcyPSS non-Darcy gas flow (with turbulence)Mscf/d
NonDarcyCoefficientEstimate D coefficient from rock/fluid propertiesdimensionless
TimeToPSSGasTime to reach pseudo-steady state (gas)hours
TimeToPSSTime to reach PSS (general, liquid)hours
DrainageRadiusEffective drainage radius from areaft
EffectiveWellboreRadiusEquivalent radius accounting for skinft
EquivalentSkinFactorEquivalent skin for hydraulic fracturesdimensionless


References

  1. Lee, J. and Wattenbarger, R.A. (1996). Gas Reservoir Engineering. SPE Textbook Series Vol. 5. Richardson, TX: Society of Petroleum Engineers.

  2. Economides, M.J., Hill, A.D., Ehlig-Economides, C., and Zhu, D. (2013). Petroleum Production Systems, 2nd Edition. Upper Saddle River, NJ: Prentice Hall. Chapter 4: Gas Well Deliverability.

  3. Ahmed, T. (2019). Reservoir Engineering Handbook, 5th Edition. Cambridge, MA: Gulf Professional Publishing. Chapter 13: Gas Well Testing.

  4. Guo, B., Lyons, W.C., and Ghalambor, A. (2007). Petroleum Production Engineering: A Computer-Assisted Approach. Burlington, MA: Gulf Professional Publishing.

  5. Jones, L.G., Blount, E.M., and Glaze, O.H. (1976). "Use of Short Term Multiple Rate Flow Tests to Predict Performance of Wells Having Turbulence." SPE-6133-MS, presented at SPE Annual Fall Technical Conference, New Orleans, LA, October 3-6.

Well Performance
well performancegas wellsdeliverabilityDarcy flownon-Darcy flowturbulenceAOFproductivityskin factor
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