ARRANGEMENT OF THE EMPENNAGE - PowerPoint PPT Presentation

1 / 15
About This Presentation
Title:

ARRANGEMENT OF THE EMPENNAGE

Description:

ARRANGEMENT OF THE EMPENNAGE Requirements: A. Slipstream / Jetstream Effects A1. The empennage must never be in the jet efflux of the engines (must be outside cone w ... – PowerPoint PPT presentation

Number of Views:153
Avg rating:3.0/5.0
Slides: 16
Provided by: MAE15
Category:

less

Transcript and Presenter's Notes

Title: ARRANGEMENT OF THE EMPENNAGE


1
ARRANGEMENT OF THE EMPENNAGE
  • Requirements
  • A. Slipstream / Jetstream Effects
  • A1. The empennage must never be in the jet efflux
    of the engines (must be outside cone w. 6 deg.
    semi-apex angle).
  • Solutions
  • A1.1 Divert the centerline of the jet.
  • A1.2 Horizontal stabilizer dihedral.
  • A2. The empennage must not be close to a jet
    efflux because the jet pumping effect will affect
    the direction of the airflow and diminish the
    stabilizing effect of the tail.
  • A3. The empennage must be as far away as possible
    from sources of noise to avoid acoustic fatigue.

2
ARRANGEMENT OF THE EMPENNAGE
  • Requirements
  • B. Stability Control
  • A1. The fin and the rudder must provide the
    counteracting YM in case of engine failure.
  • A2. The empennage must allow for a safe recovery
    from stall and spin (especially avoid deep
    stall).

3
ARRANGEMENT OF THE EMPENNAGE
  • 1. Fuselage or Fin-Mounted Stabilizer
  • Pros
  • Structural simplicity stiffness.
  • Having one surface at the tip of the other
    increases the AReff by about 50 (winglets). As
    a result, the horizontal stabilizer can increase
    the slope of the fin by about 15.
  • Cons
  • T-tails may suffer from flutter and deep stall
    problems.

4
Cessna 550
5
BAE-146
6
ARRANGEMENT OF THE EMPENNAGE
  • 2. Twin Vertical Tail
  • Pros
  • Increased effectiveness of the horizontal
    stabilizer (winglets)
  • If the fin turns out to be too large, rudder
    deflection will cause a RM as a result of the
    large vertical distance of its ac from the
    longitudinal axis of the ac. A twin vertical
    will minimize this effect (F-14, F-15, F-18).
  • If twin tail booms are used, the twin vertical is
    the only solution available (Cessna Skymaster).
  • Decreases combat vulnerability (A-10).

7
Fairchild Republic T-46A
8
F-14
9
F-15
10
F-18 Hornet
11
Cessna Skymaster
12
A-10 Warthog
13
ARRANGEMENT OF THE EMPENNAGE
  • 3. Butterfly Tail
  • Pros
  • Avoids damage to the tail when landing on
    overgrown terrain (sailplanes).
  • Keeps tail surfaces clear of the engine efflux.
  • Looks cool (V-tail Bonanza)!
  • Cons
  • Moving surfaces serve as both rudders
    (differential deflection) and elevators
    (simultaneous deflection) complicated control
    system design.

14
Thermik-Excel Vetron Sailplane
15
Beechcraft V-Tail Bonanza
Write a Comment
User Comments (0)
About PowerShow.com