Variable Factors - P-8210199

 Web www.tpub.com

Home

Information Categories
Aerographer
Automotive
Aviation
Construction
Diving
Draftsman
Engineering
Electronics
Food and Cooking
Logistics
Math
Medical
Music
Nuclear Fundamentals
Photography
Religion

BASIC FIGHTER MANEUVERING (BFM) THEORY
CHAPTER NINE
Structural Limitations
Structural limitations include both the maximum lift that can be supported by an airframe and the
maximum-g capability (varies with fuel and ordnance load). The aircraft's maximum airspeed
may also be a limiting factor during an engagement. An aircraft's VN diagram is the "picture" of
these limitations. The T-2C VN diagram may be found in NATOPS.
Thrust-to-Weight Ratio
The thrust-to-weight ratio of an aircraft is computed by dividing thrust by combat weight. This
ratio is an excellent indicator of an aircraft's performance capability going into a BFM
engagement. The higher the ratio for the aircraft, the better the energy addition rate will be. The
T-2C has a thrust-to-weight ratio less than one. Crews flying aircraft with thrust-to-weight ratios
greater than one, will use different tactics than crews flying aircraft with ratios less than one.
Wing loading is computed by dividing the combat weight of an aircraft by the wing area. For
two aircraft at the same airspeed, the aircraft with the higher wing loading will have a larger turn
radius and a faster turn rate.
In VT-86, students will be fighting other T-2Cs. For this reason, fixed factors become less
crucial as both aircraft have the same limitations. Therefore variable factors and tactics become
the deciding factors when fighting against the same model aircraft.
915. VARIABLE FACTORS
Numerous factors will constantly vary during each engagement in the BFM arena to include a
fighter's altitude, airspeed, angle of attack (AOA), and G. At any given "snapshot" in time these
variable factors present the fighter with a set of parameters requiring instantaneous analysis in
order to achieve the relative positional advantage desired. Turn radius and turn rate are two
additional variable factors that define the aircraft's turning performance.
The distance from the center point to the arc of the circle an aircraft scribes through the air
during a turn is its turn radius. Turn radius (TAS2/G) is a function of airspeed and G. At a given
G-load, an aircraft's turn radius will increase as airspeed increases. The ability to have a small
turn radius and "turn inside" the bogey can often be used to gain a positional advantage.
Turn Rate
Turn rate is the rate at which an aircraft turns (in degrees per second) and is approximated by the
simplified formula (G/TAS). Simply, an aircraft that can pull more g at a given airspeed will
have a faster turn rate than another aircraft. This gives the faster-turn-rate aircraft the ability to
get his nose on the bogey first, which can be used to gain a positional advantage.
9-9
BASIC FIGHTER MANEUVERING (BFM) THEORY

 Integrated Publishing, Inc. 6230 Stone Rd, Unit Q Port Richey, FL 34668 Phone For Parts Inquiries: (727) 493-0744 Google +