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Calculators Created by Harsh Raj

Harsh Raj
Indian Institute of Technology, Kharagpur (IIT KGP), West Bengal
54
Formulas Created
29
Formulas Verified
24
Across Categories

List of Calculators by Harsh Raj

Following is a combined list of all the calculators that have been created and verified by Harsh Raj. Harsh Raj has created 54 and verified 29 calculators across 24 different categories till date.
Aircraft Dynamics Nomenclature (1)
Verified Mean Aerodynamic Chord for Propeller-Driven Airplane
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17 More Aircraft Dynamics Nomenclature Calculators
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Area of Triangle (3)
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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17 More Area of Triangle Calculators
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Circular Orbit Parameters (1)
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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Directional Control (5)
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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Elliptical Orbit Parameters (11)
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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Expansion Waves (1)
Created Flow Deflection Angle due to Expansion Wave
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9 More Expansion Waves Calculators
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Fuselage Contribution (2)
Verified Coefficient of Pitching Moment Respect to Fuselage Contribution
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Verified Pitching Moment Coefficient for Fuselage Contribution
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Geostationary Earth Satellite (7)
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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Hperbolic Orbit Parameters (6)
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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Jet Airplane (3)
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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15 More Jet Airplane Calculators
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Landing (1)
Verified Landing Ground Run
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4 More Landing Calculators
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Lateral Control (10)
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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Lifting Flow over Cylinder (4)
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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Nonlifting Flow over Cylinder (5)
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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Nozzle Shape (2)
Verified Characteristics Velocity
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Verified Nozzle Thrust Coefficient
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1 More Nozzle Shape Calculators
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Nozzles (1)
Verified Propulsion Efficiency
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Orbital Position as Function of Time (6)
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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Orbital Position as Function of Time (4)
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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Orbital Position as Function of Time (5)
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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Parabolic Orbit Parameters (4)
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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Rocket Propulsion (1)
Verified Total Impulse
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13 More Rocket Propulsion Calculators
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Take-Off (1)
Verified Take Off Ground Run
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14 More Take-Off Calculators
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Theory Of Rockets (3)
Verified Propellent Mass Fraction
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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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6 More Theory Of Rockets Calculators
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Trigonometric Ratios of Half Angles using Sides of Triangles (9)
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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