Tspear: Draft

2016-08-16T00:42:46Z

Draft

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== Airplane List ==
{| class="wikitable"
|-
! N Number !! Model !! Engine !! Cooling Modifications !! Engine Modifications !! Propeller Type !! Gap between aft surface and prop !! Max Fuel !! Takeoff Weight
|-
| Example N || Imagination || None || alcohol || A big one || 3 blade CS || 2ft || 100gal || Example
|-
| Example || Example || Example || Example || Example || Example || Example || Example || Example
|}

== Ground Ops Params ==
{| class="wikitable"
|-
! N Number !! Airport OAT !! Wind Bearing !! 1000 RPM Diff Pressure !! 1700 RPM Diff Pressure !! Full Throttle Diff Pressure
|-
| Example || Example || Example || Example || Example || Example
|-
| Example || Example || Example || Example || Example || Example
|-
| Example || Example || Example || Example || Example || Example
|}

== Takeoff ==
Takeoff to measure initial effect of aircraft movement at the following speeds:

{| class="wikitable"
|-
! N Number !! 20 KIAS Diff Pressure !! 50 KIAS Diff Pressure !! 80 KIAS Diff Pressure
|-
| Example || Example || Example || Example
|-
| Example || Example || Example || Example
|-
| Example || Example || Example || Example
|}

== Climb ==
* Full climb power (whatever is the maximum climb power your engine type would normally be set for if you were shooting for max performance climb)
* This will record aircraft body angle (pitch) during a normal climb to see if high body angles have a great impact on cooling as the more powerful airplanes will require a higher body angle
* Should have started takeoff with full fuel and two occupants (need assistant)
* Have the autopilot (if installed/capable) fly IAS hold mode (to ensure a consistent digital reading and consistent airflow through the intake)
* Let aircraft stabilize at each intermediate IAS for 20 seconds
* Record the following data points (RPM, MP, Diff Pressure, Pitch) at the following speeds (100, 110, 120, 130, 140, 150 KIAS)

=== 100 KIAS ===
{| class="wikitable"
|-
! N Number !! RPM !! MP !! Diff Pressure !! Pitch || OAT
|-
| Example || Example || Example || Example || Example || F
|-
| Example || Example || Example || Example || Example || F
|}

=== 110 KIAS ===
{| class="wikitable"
|-
! N Number !! RPM !! MP !! Diff Pressure !! Pitch || OAT
|-
| Example || Example || Example || Example || Example || F
|-
| Example || Example || Example || Example || Example || F
|}

=== 120 KIAS ===
{| class="wikitable"
|-
! N Number !! RPM !! MP !! Diff Pressure !! Pitch || OAT
|-
| Example || Example || Example || Example || Example || F
|-
| Example || Example || Example || Example || Example || F
|}

=== 130 KIAS ===
{| class="wikitable"
|-
! N Number !! RPM !! MP !! Diff Pressure !! Pitch || OAT
|-
| Example || Example || Example || Example || Example || F
|-
| Example || Example || Example || Example || Example || F
|}

=== 140 KIAS ===
{| class="wikitable"
|-
! N Number !! RPM !! MP !! Diff Pressure !! Pitch || OAT
|-
| Example || Example || Example || Example || Example || F
|-
| Example || Example || Example || Example || Example || F
|}

=== 150 KIAS ===
{| class="wikitable"
|-
! N Number !! RPM !! MP !! Diff Pressure !! Pitch || OAT
|-
| Example || Example || Example || Example || Example || F
|-
| Example || Example || Example || Example || Example || F
|}

== Straight and Level ==
* Strait and Level Cruise at 8000 FT autopilot on ALT hold mode
* Leaned to usual cruise power (needs appropriate mixture setting for the faster speeds)
* Let aircraft stabilize at each intermediate cruise speed for 2 minutes to ensure an accurate recording of each data point

=== 120 KIAS ===
{| class="wikitable"
|-
! N Number !! RPM !! MP !! Diff Pressure !! Pitch || CHT || EGT || OAT || TAS
|-
| Example || Example || Example || Example || Example || F || F || F || k
|-
| Example || Example || Example || Example || Example || F || F || F || k
|}

=== 140 KIAS ===
{| class="wikitable"
|-
! N Number !! RPM !! MP !! Diff Pressure !! Pitch || CHT || EGT || OAT || TAS
|-
| Example || Example || Example || Example || Example || F || F || F || k
|-
| Example || Example || Example || Example || Example || F || F || F || k
|}

=== 160 KIAS ===
{| class="wikitable"
|-
! N Number !! RPM !! MP !! Diff Pressure !! Pitch || CHT || EGT || OAT || TAS
|-
| Example || Example || Example || Example || Example || F || F || F || k
|-
| Example || Example || Example || Example || Example || F || F || F || k
|}

=== 180 KIAS ===
{| class="wikitable"
|-
! N Number !! RPM !! MP !! Diff Pressure !! Pitch || CHT || EGT || OAT || TAS
|-
| Example || Example || Example || Example || Example || F || F || F || k
|-
| Example || Example || Example || Example || Example || F || F || F || k
|}

=== 200 KIAS ===
{| class="wikitable"
|-
! N Number !! RPM !! MP !! Diff Pressure !! Pitch || CHT || EGT || OAT || TAS
|-
| Example || Example || Example || Example || Example || F || F || F || k
|-
| Example || Example || Example || Example || Example || F || F || F || k
|}

Cooling Project - Revision history

Tspear: Draft