Business Jet Research Paper

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Student number: S3320134 Variant Code: A9
MISSION SPECIFICATION

A business jet

Payload: 9 passengers at 175 lbs each and 30 lbs of baggage each

Crew: 1 pilot

Range: at least 1500 nm with at least 1 hour loiter reserves for flight to an alternate airport, 100 nm away, then a 45 min loiter

Altitude: 40,000 ft for design mission

Cruise speed: 450 kts

Takeoff: FAR 25 field length 5000 ft, at 5000 ft altitude and standard day

Landing: FAR 25 field length 3000 ft, at 5000 ft, standard day, WL ≥0.85 WTO

Climb: climb to 40,000 ft in 20 min

Service ceiling: 51,000 ft

Certification: FAR 25

1. WEIGHT ESTIMATION

Methods and Results

In order to obtain the total weight of the aircraft, the …show more content…

(Eqn 2.1)

Where σ = density ratio = ρTO/ρsealevel ρTO 0.002048slug/ft3 ρsealevel 0.00238 slug/ft3 σ 0.860504

(Eqn 2.2) Table 6. Density ratio
The take-off thrust to weight ratio (T/W)TO can be calculated as follow:

-Sizing to landing
SFL= 3000ft
From (Eqn 2.3) VA can be obtained:

SFL = 0.3 VA3 VA = (3000/0.3)1/2
= 100kts

With Eqn (2.4):

Vstall = 100 / 1.3 = 76.92 kts = 79.62 x 1.68781 = 129.83 ft/s (Eqn2.5)
(W/S)L can be calculated as

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