Aircraft Design Projects for Engineering Students, by James F. Marchman, Lloyd R. Jenkinson

By James F. Marchman, Lloyd R. Jenkinson

Written for college students of aeronautical engineering and in response to a variety of distinct airplane layout initiatives, this wide-ranging e-book attracts jointly the weather of plane layout and should aid any plane layout venture. Written by means of skilled U.K. and U.S. dependent authors this can be a distinct source that opens up the preliminary layout procedure, explores the adventure of others on related initiatives, and clarifies the techniques which are in the back of the equations and calculations utilized in airplane layout. Armed with this data, readers should be freer to pay attention to the cutting edge and analytical elements in their personal undertaking paintings.

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Such methods are referred to as trade-off or sensitivity studies. They generally investigate the variation of a single parameter while keeping all others constant. Multivariable investigations are referred to as parametric studies, these are explained later in this chapter. Trade studies can take many different forms. ). g. ). g. ). All of these have the objective of building confidence in the design predictions on which the aircraft configuration is based. 10. These figures are introduced here only as examples of the type of studies that are possible.

When using the Brequet range equation it must be remembered that both engine (SFC) and aircraft (L/D) will be different for different flight conditions. These variations arise because the aircraft speed, altitude, weight and engine setting will be different for each flight segment. Typical values for (SFC) can be found in engine data books7 or from aircraft and engine textbooks4,8 for the type of engine to be used. The aircraft lift to drag ratio (L/D) will vary and be dependent on aircraft geometry (particularly wing angle of attack).

9) shows the effect of wing aspect ratio. “chap02” — 2003/3/10 — page 29 — #24 29 30 Aircraft Design Projects Fuel wt (Ib) Wing gross area (sq. 35 Fig. 8 Wing taper ratio sensitivity study (example) DOC per flight ($) Wing area (sq. ft) Op. 5 Fig. e. the influence of span loading on climb performance and the activation of the WAT (weight, altitude and temperature) restrictions at low values of aspect ratio). 32. “chap02” — 2003/3/10 — page 30 — #25 Preliminary design Gross wing area (sq.

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