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Prandtl-Meyer Supersonic Expansion Fan Function & Mach Calculator

Easily calculate and compute prandtl-meyer supersonic expansion fan function & mach calculator with accurate equations, live formulas, and expert guidance.

Calculated Result
11.91 deg

Prandtl-Meyer Function nu(M)

Prandtl-Meyer Function nu(M)

11.91 deg

Upstream Prandtl Meyer Nu1 Deg

11.905208826739662

Downstream Prandtl Meyer Nu2 Deg

23.905208826739663

Downstream Mach Number M2

1.9112934641301764

Static Pressure Ratio P2 P1

0.5383838924634715

11.91 — deg

Calculation Breakdown

  1. Applied FormulaEvaluates the Prandtl-Meyer expansion angle nu(M in deg) and computes downstream expansion Mach number (M2) and static pressure drops around sharp convex supersonic corners.\nu(M) = \sqrt{\frac{\gamma+1}{\gamma-1}} \arctan\left(\sqrt{\frac{\gamma-1}{\gamma+1}(M^2-1)}\right) - \arctan\left(\sqrt{M^2-1}\right)

Prandtl-Meyer Expansion Fan Metric Output

Interactive visualization based on your current inputs

Calculated Value
0.03.06.08.912Prandtl-Meyer Function nu(M)

What Is the Prandtl-Meyer Supersonic Expansion Fan Function & Mach Calculator?

The Prandtl-Meyer Supersonic Expansion Fan Function & Mach Calculator computes results using established domain formulas, verified conversion factors, and user-entered parameters.

How Does the Prandtl-Meyer Supersonic Expansion Fan Function & Mach Calculator Work?

Evaluates the Prandtl-Meyer expansion angle nu(M in deg) and computes downstream expansion Mach number (M2) and static pressure drops around sharp convex supersonic corners.

Prandtl-Meyer Supersonic Expansion Fan Function & Mach Calculator Formula & Variables

The core mathematical equation utilized by this calculator is expressed as:

ν(M)=γ+1γ−1arctan⁡(γ−1γ+1(M2−1))−arctan⁡(M2−1)\nu(M) = \sqrt{\frac{\gamma+1}{\gamma-1}} \arctan\left(\sqrt{\frac{\gamma-1}{\gamma+1}(M^2-1)}\right) - \arctan\left(\sqrt{M^2-1}\right)

Evaluates the Prandtl-Meyer expansion angle nu(M in deg) and computes downstream expansion Mach number (M2) and static pressure drops around sharp convex supersonic corners.

How to Use the Prandtl-Meyer Supersonic Expansion Fan Function & Mach Calculator

  1. Enter your parameters into the designated input fields to calculate the result immediately.

Step-by-Step Example Calculation

Prandtl-Meyer Supersonic Expansion Fan Function & Mach Calculator Example

Input Values:

upstreamMachNumberM1:1.5
cornerDeflectionAngleDeg:12
specificHeatRatioGamma:1.4
Worked Steps: Sample evaluation based on standard reference conditions.

Understanding Your Result

The calculated primary figure indicates the optimal or required deg.

Factors That Affect the Result

  • Measurement tolerances, operational variance, and real-world conditions.

When Should You Use This Calculator?

  • Everyday budgeting, technical homework, professional estimation, and household projects.

Assumptions & Limitations

  • Assumes standard atmospheric or environmental parameters unless specified.

Frequently Asked Questions

Calculation Accuracy & Reference Note

Double-precision IEEE 754 arithmetic with validated empirical constants.

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