Quick Summary: Geometric angles of attack measured were [-10, -6, -3, 0, 3, 6, 10, 13, 15, 16, 19, 20] degrees; The following video gives a short demonstration of collecting and analyzing

Wind Tunnel Pressure Data For A Naca 0012 Symmetric Airfoil - Planning Snapshot

Overview

Geometric angles of attack measured were [-10, -6, -3, 0, 3, 6, 10, 13, 15, 16, 19, 20] degrees; The following video gives a short demonstration of collecting and analyzing

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Important details found

  • Geometric angles of attack measured were [-10, -6, -3, 0, 3, 6, 10, 13, 15, 16, 19, 20] degrees;
  • The following video gives a short demonstration of collecting and analyzing

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Image References

Wind tunnel pressure data for a NACA 0012 symmetric airfoil
NACA 0012 Wind Tunnel Testing
NACA 0012 airfoil pressure coefficient distribution from low-speed wind tunnel data
Tiny wind tunnel: NACA 0012 - Pressure field
2024x1024 wind tunnel: NACA 0012 - Pressure field
Wind Tunnel with NACA 0012, Transient. -0.4 rad/s
Group 3 - NACA 0012 Lab experiment
NACA 0012 Wind Tunnel Testing
airfoil 3 wind tunnel
flow visualization of an airfoil in wind tunnel
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Wind tunnel pressure data for a NACA 0012 symmetric airfoil

Wind tunnel pressure data for a NACA 0012 symmetric airfoil

The following video gives a short demonstration of collecting and analyzing

NACA 0012 Wind Tunnel Testing

NACA 0012 Wind Tunnel Testing

Read more details and related context about NACA 0012 Wind Tunnel Testing.

NACA 0012 airfoil pressure coefficient distribution from low-speed wind tunnel data

NACA 0012 airfoil pressure coefficient distribution from low-speed wind tunnel data

Geometric angles of attack measured were [-10, -6, -3, 0, 3, 6, 10, 13, 15, 16, 19, 20] degrees;

Tiny wind tunnel: NACA 0012 - Pressure field

Tiny wind tunnel: NACA 0012 - Pressure field

Read more details and related context about Tiny wind tunnel: NACA 0012 - Pressure field.

2024x1024 wind tunnel: NACA 0012 - Pressure field

2024x1024 wind tunnel: NACA 0012 - Pressure field

Read more details and related context about 2024x1024 wind tunnel: NACA 0012 - Pressure field.

Wind Tunnel with NACA 0012, Transient. -0.4 rad/s

Wind Tunnel with NACA 0012, Transient. -0.4 rad/s

Read more details and related context about Wind Tunnel with NACA 0012, Transient. -0.4 rad/s.

Group 3 - NACA 0012 Lab experiment

Group 3 - NACA 0012 Lab experiment

Read more details and related context about Group 3 - NACA 0012 Lab experiment.

NACA 0012 Wind Tunnel Testing

NACA 0012 Wind Tunnel Testing

Read more details and related context about NACA 0012 Wind Tunnel Testing.

airfoil 3 wind tunnel

airfoil 3 wind tunnel

Read more details and related context about airfoil 3 wind tunnel.

flow visualization of an airfoil in wind tunnel

flow visualization of an airfoil in wind tunnel

Read more details and related context about flow visualization of an airfoil in wind tunnel.