Static and Dynamic Response of a Design of Differential ... - aerade

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oo7r-- I 0 06 I ,c I 0 05 - 004 *P P, 003 0 “T--Y I I / I Ap - PRESSURE OIFFERENCE BE~-~vEEN HOLES ps= FREE STREAM STATIC PRESSURE I I / 2 IV’= P,-Ps OF WATER) FlG.20. PRESSURE DIFFERENCE DUE TO AN INDEPENDENT (SUBSONIC) CROSS FCOW VELOCITY. / l t
SMALL, OP, $ OP YAWMETER AXIS FIG.21. GEOMETRIC RELATIONS BETWEEN INDICATED AND TRUE INCIDENCE AND ROLL ANGLE.
Page 1:
c. Pi.$-lj 4 I4 A.R.C. TechnIcal Re
Page 5 and 6:
List of Syrdmls 1 Introduction 2 Te
Page 7 and 8:
3 a *I *2 c1 c2 a.n.r. g(s) G(S) i
Page 9: 3 Superscriots . L at Other suffice
Page 12 and 13: This type of instrument has the dis
Page 14 and 15: P = Pa-c y (Po - ps) sin*$ where ps
Page 16 and 17: 3-$ calibres behind the nose in acc
Page 18 and 19: which zmounw ?;o assvr;lin~ thzt si
Page 20 and 21: where the factor 0.22, applicable t
Page 22 and 23: In the present c&se z, = LqS + RI z
Page 24 and 25: The value for v is given by the dif
Page 26 and 27: a = speed of sound in air in the tu
Page 28 and 29: is thus reduced to the determinntio
Page 30 and 31: corresponding to a maximum volume c
Page 32 and 33: would be always m the same sense. T
Page 34 and 35: well, then If the pressure, ppit, f
Page 37: Effect of inaccurate pressure hole
Page 40 and 41: Thus the reqtianent is satisfied pr
Page 42 and 43: &thod 2 Alternatively we may use eq
Page 44 and 45: 4.0.- 3.! j- 2 15 3. O- 2, 5- 2. o-
Page 46 and 47: t----PLANE 1 CI I I I I I I I I I -
Page 48 and 49: 90 p. : STAGNATION PRESSURE FEWIN A
Page 50 and 51: 35 30 AP P, 25 25 3 FIG 9 (b) 0, =
Page 52: VO- I.0 ‘5 = ACWSTI~ DAMPING FACT
Page 55 and 56: 1 , FIG 15. PRESSURE RESPONSE OF YA
Page 58 and 59: FIG 18 TIME LAG OF INTERIM (LONG TU
Page 64: 0 Crown Copyright 1958 Pubhshed by
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Static and Dynamic Response of a Design of Differential ... - aerade

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