Two points (4, p) and (0, q) lie on a straight line having a slope of 3/4. The

Question

Two points (4, p) and (0, q) lie on a straight line having a slope of 3/4. The value of (p “ q) is

Options:

A . -3

B . 0

C . 3

D . 4

Answer: Option C

-NA-

Was this answer helpful ?

Next Question

More Questions on This Topic :

Question 1. A vortex flowmeter works on the principle that the Strouhal number of 0.2 is a constant over a wide range of flow rates....then the velocity of the flow would be measured as

Question 2. The propellant in a single stage sounding rocket occupies 60% of its initial mass. If all of it is expended instantaneo....acceleration due to gravity to be constant at 9.81 m/s2.]

Question 3. A bipropellant liquid rocket motor operates at a chamber pressure of 40 bar with a nozzle throat diameter of 50 mm. The....tank volume for a burn time of 8 minutes

Question 4. The stagnation temperatures at the inlet and exit of a combustion chamber are 600 K and 1200 K, respectively. If the he....1.005 kJ/kg.K and 1.147 kJ/kg.K respectively, the fuel-to-air ratio is

Question 5. A solid propellant of density 1800 kg/m3 has a burning rate law r = 6.65 x 10-3p0.45 mm/s, where p is pressure in Pasca....of 50 bar at the end of the ignition transient?

Question 6. The Airy stress function, Ï† =Î± x2 +Î² xy +Î³ y2 for a thin square panel of size l Ã—l automatically satis....all four edges, the traction boundary conditions are satisfied by

Question 7. Buckling of the fuselage skin can be delayed by ....

Question 8. A spring-mass system is viscously damped with a viscous damping constant c. The energy dissipated per cycle when the sy....is undergoing a harmonic vibration X CosÏ‰dt is given by

Question 9. The boundary condition of a rod under longitudinal vibration is changed from fixed-fixed to fixedfree. The fundamental ....is now k times the original frequency, where k is

Question 10. A wing and tail are geometrically similar, while tail area is one-third of the wing area and distance between two aerod....be behind aerodynamic centre without destabilizing the wing-tail combination is

Chapter 1 - GLOBAL STEEL SCENARIO & INDIAN STEEL INDUSTRY Part 1 : (13-04-2024) INDUSTRY AND COMPANY AWARENESS (ICA)

Direction Sense Test Part 1 Reasoning (Hindi)

Chapter 1 - RMHP / OHP / OB & BP Part 1 : (14-02-2024) GPOE

Cube & Cuboid Part 1 Reasoning (Hindi)

Data Interpretation (DI) Basic Concept Reasoning (Hindi)

Counting Figures Part 1 Counting Of Straight Lines Reasoning (Hindi)

Sail E0 free webinar Webinars

Real Numbers Part 7 Class 10 Maths

Real Numbers Part 1 Class 10 Maths

Polynomials Part 1 Class 10 Maths

DSP Combined 1 Free Revision Test SAIL JO E-0

GPOE / GPA Combined 1 Free Revision Test SAIL JO E-0

BSP Plant Specific Review Test SAIL JO E-0

BSL Combined 1 Free Revision Test SAIL JO E-0

GFM Combined 1 Free Revision Test SAIL JO E-0