Wing Reference Area for given Horizontal Tail Volume Ratio Calculator

✖The Horizontal Tail Moment Arm is the distance between the lift center of the horizontal tail and the center of gravity of the aircraft.ⓘ Horizontal Tail Moment Arm [𝒍_t]			+10% -10%
✖The Horizontal Tail Area is the surface area of the horizontal stabilizer on an aircraft, which provides pitch stability and control.ⓘ Horizontal Tail Area [S_t]			+10% -10%
✖Horizontal Tail Volume Ratio relates the area of the horizontal tail, the distance between tail and aircraft's c.g., the wing area, and the mean aerodynamic wing chord.ⓘ Horizontal Tail Volume Ratio [V_H]			+10% -10%
✖The Mean Aerodynamic Chord is a two-dimensional representation of the whole wing.ⓘ Mean Aerodynamic Chord [c_ma]			+10% -10%

✖The Reference Area is arbitrarily an area that is characteristic of the object being considered. For an aircraft wing, the wing's planform area is called the reference wing area or simply wing area.ⓘ Wing Reference Area for given Horizontal Tail Volume Ratio [S]

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Wing Reference Area for given Horizontal Tail Volume Ratio Solution

STEP 0: Pre-Calculation Summary

Formula Used

Reference Area = Horizontal Tail Moment Arm*Horizontal Tail Area/(Horizontal Tail Volume Ratio*Mean Aerodynamic Chord)
S = 𝒍_t*S_t/(V_H*c_ma)
This formula uses 5 Variables

Variables Used

Reference Area - (Measured in Square Meter) - The Reference Area is arbitrarily an area that is characteristic of the object being considered. For an aircraft wing, the wing's planform area is called the reference wing area or simply wing area.
Horizontal Tail Moment Arm - (Measured in Meter) - The Horizontal Tail Moment Arm is the distance between the lift center of the horizontal tail and the center of gravity of the aircraft.
Horizontal Tail Area - (Measured in Square Meter) - The Horizontal Tail Area is the surface area of the horizontal stabilizer on an aircraft, which provides pitch stability and control.
Horizontal Tail Volume Ratio - Horizontal Tail Volume Ratio relates the area of the horizontal tail, the distance between tail and aircraft's c.g., the wing area, and the mean aerodynamic wing chord.
Mean Aerodynamic Chord - (Measured in Meter) - The Mean Aerodynamic Chord is a two-dimensional representation of the whole wing.

STEP 1: Convert Input(s) to Base Unit

Horizontal Tail Moment Arm: 0.801511 Meter --> 0.801511 Meter No Conversion Required
Horizontal Tail Area: 1.8 Square Meter --> 1.8 Square Meter No Conversion Required
Horizontal Tail Volume Ratio: 1.42 --> No Conversion Required
Mean Aerodynamic Chord: 0.2 Meter --> 0.2 Meter No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

S = 𝒍_t*S_t/(V_H*c_ma) --> 0.801511*1.8/(1.42*0.2)

Evaluating ... ...

S = 5.07999929577465

STEP 3: Convert Result to Output's Unit

5.07999929577465 Square Meter --> No Conversion Required

FINAL ANSWER

5.07999929577465 ≈ 5.079999 Square Meter <-- Reference Area

(Calculation completed in 00.004 seconds)

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Created by Vinay Mishra

Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune

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Indian Institute of Technology (IIT), Bombay

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Wing Reference Area for given Horizontal Tail Volume Ratio Formula

LaTeX Go

Reference Area = Horizontal Tail Moment Arm*Horizontal Tail Area/(Horizontal Tail Volume Ratio*Mean Aerodynamic Chord)
S = 𝒍_t*S_t/(V_H*c_ma)

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Taper ratio is one of the parameters on planform geometry, which means the ratio of the wing's root and tip chord lengths. Hence, its effects on the wing's aerodynamic parameters are also essential and should be considered during a wing design process.

How to Calculate Wing Reference Area for given Horizontal Tail Volume Ratio?

Wing Reference Area for given Horizontal Tail Volume Ratio calculator uses Reference Area = Horizontal Tail Moment Arm*Horizontal Tail Area/(Horizontal Tail Volume Ratio*Mean Aerodynamic Chord) to calculate the Reference Area, Wing Reference Area for given Horizontal Tail Volume Ratio is a measure of the wing's reference area, calculated by multiplying the horizontal tail's moment arm and area, and dividing by the product of the horizontal tail volume ratio and mean aerodynamic chord. Reference Area is denoted by S symbol.

How to calculate Wing Reference Area for given Horizontal Tail Volume Ratio using this online calculator? To use this online calculator for Wing Reference Area for given Horizontal Tail Volume Ratio, enter Horizontal Tail Moment Arm (𝒍_t), Horizontal Tail Area (S_t), Horizontal Tail Volume Ratio (V_H) & Mean Aerodynamic Chord (c_ma) and hit the calculate button. Here is how the Wing Reference Area for given Horizontal Tail Volume Ratio calculation can be explained with given input values -> 5.079999 = 0.801511*1.8/(1.42*0.2).

FAQ

What is Wing Reference Area for given Horizontal Tail Volume Ratio?

Wing Reference Area for given Horizontal Tail Volume Ratio is a measure of the wing's reference area, calculated by multiplying the horizontal tail's moment arm and area, and dividing by the product of the horizontal tail volume ratio and mean aerodynamic chord and is represented as S = 𝒍_t*S_t/(V_H*c_ma) or Reference Area = Horizontal Tail Moment Arm*Horizontal Tail Area/(Horizontal Tail Volume Ratio*Mean Aerodynamic Chord). The Horizontal Tail Moment Arm is the distance between the lift center of the horizontal tail and the center of gravity of the aircraft, The Horizontal Tail Area is the surface area of the horizontal stabilizer on an aircraft, which provides pitch stability and control, Horizontal Tail Volume Ratio relates the area of the horizontal tail, the distance between tail and aircraft's c.g., the wing area, and the mean aerodynamic wing chord & The Mean Aerodynamic Chord is a two-dimensional representation of the whole wing.

How to calculate Wing Reference Area for given Horizontal Tail Volume Ratio?

Wing Reference Area for given Horizontal Tail Volume Ratio is a measure of the wing's reference area, calculated by multiplying the horizontal tail's moment arm and area, and dividing by the product of the horizontal tail volume ratio and mean aerodynamic chord is calculated using Reference Area = Horizontal Tail Moment Arm*Horizontal Tail Area/(Horizontal Tail Volume Ratio*Mean Aerodynamic Chord). To calculate Wing Reference Area for given Horizontal Tail Volume Ratio, you need Horizontal Tail Moment Arm (𝒍_t), Horizontal Tail Area (S_t), Horizontal Tail Volume Ratio (V_H) & Mean Aerodynamic Chord (c_ma). With our tool, you need to enter the respective value for Horizontal Tail Moment Arm, Horizontal Tail Area, Horizontal Tail Volume Ratio & Mean Aerodynamic Chord and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

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