Introduction to flight anderson manual solution pdf

Introduction to flight anderson manual solution pdf

2. sen i 0052

4. y= Fore dto pese (1p dc f (2116-105) de
2116 «Se = 6503 I pepe va

Fo due bras [1 den [as

res
Gao

5. repetía he fes dirt.

6. xd

11. Also fom Appendix B, py = 21162 IM tse ee, nd T= 29.64 a 25000

42 101 103001/=-101x10 Wn por mino

13. [epa

16. ro

Asda se ug Hees,

Voss =a” 7

19. prom Us BEN

21. Since the fw is sa ip,

24. Note that te nae of poem 4.11 ist bay span

un ¡RT

toe

25. yin gy orc.

27. I Tesi sy en

31. tt peaks a tglyspemonis Mach number, ad then decrees as te ste
430. Rec at total presse defined as that peas tat woul exist if the low
wer slowed epi 0 zr veloc Ths i denon ple al flows

pres of res, a callate above. This stagnation pre the nos of a

34. AZAR 46 18 20

M

38. ow pve bythe Euler ua, Eq.)

wy

to achieve given pesnage chang in veoi thn fora low speed flow, eventing

39. 2 fiea2 00] = 28710"

40. ln proc, reservoir ters of ot hl is vals o es employed wid the

42. 2, Of arial nares sth the xt soi io by a ry sll
doubled, The Higher Mach umber of 20 is achieved ot by a arg nr in
wenn peri wind tenes be higher Mach

45. 4644 (9) Forte fw, Cea hs. Since Re

50. Checking te Repnoós ber, min the viso seien fom the carve

51. 4001, which is about 10 pcs higher than te val of 0.09 given fr Re 3.x 1

53. ETS

55. R „ung,

57. couse, where

59. sa uivenal cane, and ence un be use or this and all or problems. We simply
acto oi th vation of Cy wth Ma om he Prand Gar rl a follows:

60. Pease not tht, comping problems 515 and 516, cial Mach number fr a given

61. Lave igh ia’ mus balance wg, Bene

62. = 002 ans (or 12 does)

65. ger ha at high speed, nar mai vlc. Compare resto problems $20

67. (0166-0)

70. FI CRD

Hens, bene val FLD i

74. Fr ey,
Che)

76. These mach mans ae shy rer han what might be he ata dr dieran

78. E

E

3

El

to do da ate do sto do Va
Pilsee)

79. Pam Ovo)? nn,

The power ented an poner ala carves ae lod below

80. ZA

Te ato ats SE, (Oh)

82. number fanion made byte sea. For example ithe P ce icons
onthe sde answers is here avid, In my on eperkne, am glad when the

83. ESO

Henos:Co=20.03)-0016

(1y _[etoyer2yoa)

84. 210) (28)

Ress

88. 16. AR=WS, enced = (STAR = (CES = 748m

90. Vimenes

‘Sic thei 2er er todo, Co = €

ZI 0-0)

07 p= $008 ae

91. oz

92. From the quad

95. ating verily upward, ad 631051 Ib. As Mach one, the ng fir exceeds the
maximum downward fre Hens, I a posible or th plane to ace Mach

98. 004107093)

99. Aer i he moment oii aout it

Atte th ang of tack,

101. nt [nv

au +005 00-2022) -00

102. oon (oo2-cosf 22)

103. By dei

104. ais" aor)

105. Thisis tobe compared with Cy, 0139 fn Proben 7 fork ined ai

1]

Note tu mar fr fr is 79% o at o siii

This to be compared with a ope of 0.039 bain rom Poe 7. or te ick

107. yale, he center of

V2/3 m/sec

110. oF

Jean

re

hen Fan
Gates

Mare Vo AT III TO = 0 x 10 ae = 5.02 moe

114. Ve

The aso i moving a 0.9 tines the esas voi fom th un.

115. Aide topos = 68347 1064 x 10 = 04367 x tom = SET

116. BAL The angle momentum per nt mas he, To alt posed as

b= 5196510

117. Ver 0 (6817 10 (11182 10%) = 76 ms = PETER

120. a}

PA = (04694045400) kgs

126. ator x 109+ [rs

128. 0 i: og (009)=Ioga +n og (5

130. seña poner

132. ‘high compared he veloc ofthe rocket, m and pis ow

Tre tense sess 19. 19999 1/1

133. -—— 6.7907 —

135. This rail dementes ht boundary layers at penal Mach mts can be

very thik

136. (400K. This is

ua] |

Conn he Bont) Er rue

139. ‘ht ton dg is one-hit dag.