Calculators Created by Harsh Raj

Verified Mean Aerodynamic Chord for Propeller-Driven Airplane

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17 More Aircraft Dynamics Nomenclature Calculators

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Verified Area of Triangle given Side A and Cosec of All Three Angles

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Verified Area of Triangle given Side B and Cosec of All Three Angles

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Verified Area of Triangle given Side C and Cosec of All Three Angles

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Verified Area of Triangle using Sides A and B and Cosec of Angle C

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Verified Area of Triangle using Sides A and C and Cosec of Angle B

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Verified Area of Triangle using Sides B and C and Cosec of Angle A

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14 More Area of Triangle Calculators

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Verified Area of Triangle using Sides A, B and Cosec (C/2) and Cos (C/2)

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Verified Area of Triangle using Sides A, B and Cosec (C/2) and Sec (C/2)

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Verified Area of Triangle using Sides A, B and Cot (C/2) and Cos (C/2)

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Verified Area of Triangle using Sides A, B and Sin (C/2) and Cot (C/2)

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Verified Area of Triangle using Sides A, B and Sin (C/2) and Sec (C/2)

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Verified Area of Triangle using Sides A, B and Sin (C/2) and Tan (C/2)

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Verified Area of Triangle using Sides A, B and Tan (C/2) and Cos (C/2)

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Verified Area of Triangle using Sides A, C and Cosec (B/2) and Cos (B/2)

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Verified Area of Triangle using Sides A, C and Cosec (B/2) and Sec (B/2)

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Verified Area of Triangle using Sides A, C and Cot (B/2) and Cos (B/2)

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Verified Area of Triangle using Sides A, C and Sin (B/2) and Cot (B/2)

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Verified Area of Triangle using Sides A, C and Sin (B/2) and Sec (B/2)

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Verified Area of Triangle using Sides A, C and Sin (B/2) and Tan (B/2)

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Verified Area of Triangle using Sides A, C and Tan (B/2) and Cos (B/2)

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Verified Area of Triangle using Sides B, C and Cosec (A/2) and Cos (A/2)

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Verified Area of Triangle using Sides B, C and Cosec (A/2) and Sec (A/2)

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Verified Area of Triangle using Sides B, C and Cot (A/2) and Cos (A/2)

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Verified Area of Triangle using Sides B, C and Sin (A/2) and Cot (A/2)

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Verified Area of Triangle using Sides B, C and Sin (A/2) and Sec (A/2)

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Verified Area of Triangle using Sides B, C and Sin (A/2) and Tan (A/2)

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Verified Area of Triangle using Sides B, C and Tan (A/2) and Cos (A/2)

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3 More Area of Triangle using Trigonometric Ratios of Half Angles Calculators

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Created Speed of Satellite in Circular LEO as Function of Altitude

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10 More Circular Orbit Parameters Calculators

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Verified Rudder Control Effectiveness

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Verified Rudder Deflection Angle given Yawing Moment Coefficient

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Verified Yawing Moment Coefficient given Rudder Deflection

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Verified Yawing Moment given Rudder Deflection

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Verified Yawing Moment with Rudder Deflection Angle

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Created Angular Momentum in Elliptic Orbit Given Apogee Radius and Apogee Velocity

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Created Angular Momentum in Elliptic Orbit Given Perigee Radius and Perigee Velocity

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Created Apogee Radius of Elliptic Orbit Given Angular Momentum and Eccentricity

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Created Apogee Velocity in Elliptic Orbit Given Angular Momentum and Apogee Radius

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Created Azimuth-Averaged Radius Given Apogee and Perigee Radii

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Created Eccentricity of Elliptical Orbit given Apogee and Perigee

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Created Elliptical Orbit Time Period given Angular Momentum and Eccentricity

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Created Radial Velocity in Elliptic Orbit given Radial Position and Angular Momentum

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Created Radial Velocity in Elliptic Orbit given True Anomaly, Eccentricity, and Angular Momentum

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Created Semimajor Axis of Elliptic Orbit given Apogee and Perigee Radii

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Created True Anomaly in Elliptic Orbit Given Radial Position, Eccentricity, and Angular Momentum

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6 More Elliptical Orbit Parameters Calculators

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Verified Energy Stored in Capacitor given Charge and Voltage

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6 More Energy Density and Energy Stored Calculators

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Verified Edge Length of Equilateral Square Pyramid given Height

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Verified Edge Length of Equilateral Square Pyramid given Surface Area

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Verified Edge Length of Equilateral Square Pyramid given Volume

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Verified Height of Equilateral Pyramid given TSA

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Verified Height of Equilateral Square Pyramid given Volume

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Verified Volume of Equilateral Square Pyramid given Height

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Verified Volume of Equilateral Square Pyramid given Surface Area

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3 More Equilateral Square Pyramid Calculators

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Created Flow Deflection Angle due to Expansion Wave

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9 More Expansion Waves Calculators

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Verified Coefficient of Pitching Moment Respect to Fuselage Contribution

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Verified Pitching Moment Coefficient for Fuselage Contribution

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Created Absolute Angular Velocity given Geo Radius of Earth and Geo Speed

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Created Absolute Angular Velocity of Earth given Geo Radius

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Created Geo Radius given Absolute Angular Velocity of Earth

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Created Geo Radius given Absolute Angular Velocity of Earth and Geo Speed

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Created Geo Radius given Speed of Satellite in its Circular Geo Orbit

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Created Geo Speed along its Circular Path given Absolute Angular Velocity of Earth

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Created Speed of Satellite in its Circular GEO of Radius

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Created Aiming Radius in Hyperbolic Orbit given Semi-Major Axis and Eccentricity

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Created Perigee Radius of Hyperbolic Orbit given Angular Momentum and Eccentricity

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Created Radial Position in Hyperbolic Orbit given Angular Momentum, True Anomaly, and Eccentricity

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Created Semi-Major Axis of Hyperbolic Orbit given Angular Momentum and Eccentricity

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Created True Anomaly of Asymptote in Hyperbolic Orbit given Eccentricity

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Created Turn Angle given Eccentricity

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Verified Average Value Range Equation

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Verified Breguet Endurance Equation

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Verified Constant Speed Cruise using Range Equation

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14 More Jet Airplane Calculators

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Verified Landing Ground Run

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4 More Landing Calculators

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Verified Aileron Control Effectiveness given Aileron Deflection

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Verified Aileron Deflection given Aileron Lift Coefficient

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Verified Aileron Section lift Coefficient given Aileron Deflection

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Verified Aileron Section Lift Coefficient given Control Effectiveness

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Verified Deflection Angle given Lift Coefficient

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Verified Lift Coefficient Slope Roll Control

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Verified Lift Coefficient with respect to Roll Rate

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Verified Lift given Roll Rate

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Verified Roll Control Power

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Verified Roll Damping Coefficient

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Created Angular Position given Radial Velocity for Lifting Flow over Circular Cylinder

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Created Angular Position of Stagnation Point for Lifting Flow over Circular Cylinder

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Created Freestream Velocity given 2-D Lift Coefficient for Lifting Flow

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Created Radius of Cylinder for Lifting Flow

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6 More Lifting Flow over Cylinder Calculators

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Created Angular Position given Pressure Coefficient for Non-Lifting Flow over Circular Cylinder

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Created Angular Position given Radial Velocity for Non-Lifting Flow over Circular Cylinder

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Created Angular Position given Tangential Velocity for Non-Lifting Flow over Circular Cylinder

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Created Doublet Strength given Radius of Cylinder for Non-Lifting Flow

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Created Freestream Velocity given Doublet Strength for Non-Lifting Flow over Circular Cylinder

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5 More Nonlifting Flow over Cylinder Calculators

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Verified Area Ratio of Nozzles

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Verified Characteristics Velocity

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Verified Nozzle Thrust Coefficient

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Verified Propulsion Efficiency

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Verified Specific Temperature at Throat

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Verified Specific Volume at Throat

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Created Eccentric Anomaly in Elliptic Orbit given True Anomaly and Eccentricity

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Created Mean Anomaly in Elliptic Orbit given Eccentric Anomaly and Eccentricity

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Created Mean Anomaly in Elliptic Orbit given Time since Periapsis

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Created Time since Periapsis in Elliptic Orbit given Eccentric Anomaly and Time Period

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Created Time since Periapsis in Elliptic Orbit given Mean Anomaly

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Created True Anomaly in Elliptic Orbit given Eccentric Anomaly and Eccentricity

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Created Mean Anomaly in Parabolic Orbit given Time since Periapsis

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Created Mean Anomaly in Parabolic Orbit given True Anomaly

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Created Time since Periapsis in Parabolic Orbit given Mean Anomaly

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Created True Anomaly in Parabolic Orbit given Mean Anomaly

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Created Hyperbolic Eccentric Anomaly given Eccentricity and True Anomaly

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Created Mean Anomaly in Hyperbolic Orbit given Hyperbolic Eccentric Anomaly

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Created Time since Periapsis in Hyperbolic Orbit given Hyperbolic Eccentric Anomaly

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Created Time since Periapsis in Hyperbolic Orbit given Mean Anomaly

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Created True Anomaly in Hyperbolic Orbit given Hyperbolic Eccentric Anomaly and Eccentricity

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Created Angular Momentum given Perigee Radius of Parabolic Orbit

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Created Perigee Radius of Parabolic Orbit given Angular Momentum

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Created Radial Position in Parabolic Orbit given Angular Momentum and True Anomaly

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Created True Anomaly in Parabolic Orbit given Radial Position and Angular Momentum

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6 More Parabolic Orbit Parameters Calculators

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Verified Fuel Mass Flow rate

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Verified Oxidizer Mass Flow Rate

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Verified Propellant Mass Flow Rate

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Verified Propellant Mixture Ratio

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Verified Take Off Ground Run

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14 More Take-Off Calculators

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Verified Cot (A-B)/2 given Tan C/2

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Verified Cot (B-C)/2 given Tan A/2

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Verified Cot (C-A)/2 given Tan B/2

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7 More Tangent Rule or Napier's Analogy Calculators

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Verified Effective Exhaust Velocity of Rocket

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Verified Mass Ratio of Rocket

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Verified Payload Mass Fraction

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Verified Propellent Mass Fraction

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Verified Rocket Exhaust Gas Velocity

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Verified Structural Mass Fraction

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Verified Throat Velocity of Nozzle

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Verified Total Velocity Required to Place Satellite in Orbit

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Verified Velocity Increment of Rocket

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Verified Total Impulse

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13 More Thrust and Power Generation Calculators

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Verified Cos (A/2) given Sides B and C and Sin (A/2)

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Verified Cos (B/2) given Sides A and C and Sin (B/2)

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Verified Cos (C/2) given Sides A and B and Sin (C/2)

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Verified Sin (A/2) given Sides B and C and Cos (A/2)

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Verified Sin (A/2) given Sides B and C and Sec (A/2)

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Verified Sin (B/2) given Sides A and C and Cos (B/2)

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Verified Sin (B/2) given Sides A and C and Sec (B/2)

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Verified Sin (C/2) given Sides A and B and Cos (C/2)

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Verified Sin (C/2) given Sides A and B and Sec (C/2)

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Verified Cosec (A/2) using Sides and Semi-Perimeter of Triangle

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Verified Cosec (B/2) using Sides and Semi-Perimeter of Triangle

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Verified Cosec (C/2) using Sides and Semi-Perimeter of Triangle

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Verified Cot (A/2) using Sides and Semi-Perimeter of Triangle

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Verified Cot (B/2) using Sides and Semi-Perimeter of Triangle

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Verified Cot (C/2) using Sides and Semi-Perimeter of Triangle

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Verified Sec (A/2) using Sides and Semi-Perimeter of Triangle

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Verified Sec (B/2) using Sides and Semi-Perimeter of Triangle

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Verified Sec (C/2) using Sides and Semi-Perimeter of Triangle

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9 More Trigonometric Ratios of Half Angles using Sides of Triangles Calculators

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Verified Cos A using Area and Sides B and C of Triangle

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Verified Cos B using Area and Sides A and C of Triangle

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Verified Cos C using Area and Sides A and B of Triangle

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Verified Cosec A using Area and Sides B and C of Triangle

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Verified Cosec B using Area and Sides A and C of Triangle

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Verified Cosec C using Area and Sides A and B of Triangle

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Verified Cot A using Area and Sides B and C of Triangle

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Verified Cot B using Area and Sides A and C of Triangle

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Verified Cot C using Area and Sides A and B of Triangle

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Verified Sec A using Area and Sides B and C of Triangle

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Verified Sec B using Area and Sides A and C of Triangle

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Verified Sec C using Area and Sides A and B of Triangle

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Verified Tan A using Area and Sides B and C of Triangle

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Verified Tan B using Area and Sides A and C of Triangle

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Verified Tan C using Area and Sides A and B of Triangle

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3 More Trigonometric Ratios using Sides and Area of Triangle Calculators

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List of Calculators by Harsh Raj