commercial and military aircraft line drawings

8/9/2019 Commercial and Military Aircraft Line Drawings

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Centurion (top)


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Centurion (front)

Centurion (side)


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35


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300"143.6"

504"

Maximum diameter = 60"Forward static

pressure or ifices

57"


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Free floating slat

D-558-IIwing configurations

Wing-fenceBasic wing Wing-fence (2) Wing-fence/slat

Fixed slat Leading-edgechord extension


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Trailing edgeflap control


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Wingtip accelerometers

Leading edgeflap control

Push-pull tubeslongitudinal control

Aircraft pitchrate gyros

Aircraft normalaccelerometers

Wingtip accelerometers

First sybendi

Stabilonsurface

F

Control sticks

Pitch damperPitch stick transducersPitch feel springSeries trim actuator

M

p

M


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18.67 ft

837


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32.5 ft


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54.2 ft


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8 4 0


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8 4 5


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8 4 5


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804

NA

Separated flo w Attached flo w


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HL-10 HL-10 modified

Cambered leading edg e

N A S A


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N O R T H R O P

R E S C U E

8 0 4

B E W A R E O F B L A S T

Top hatch


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Wing flap Rudder

Bodyflaps

Helios (front)


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Helios (side)

247'

Helios (top)


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LoFLYTEAircraft Configuration


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Top view

Length: 8 ft 4 in.

Weight: 70 lbs

Performance:

Maximum speed240 knots


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N A C A


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N A C


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803

NASA

NOR THR OP


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I

II

8

14

16

19

22

28

Identification Key for :

"Celebrating One Hundred Years of Powered Flight 1903-2003" by Dr. Robert T. McCall 2003Medium: oil on canvas Dimensions: 6 feet by 18 feet Commissioned by NASA Dryden Flight Research Center, Edwards, CA.


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I

CBA EC

14

3

5

26

7 11

10

9

8

17

18

13

1215

20

21 24

25

23 27

26

29

Central Quote:"It is my belief that flight is possible..."

Wilbur Wright September 3rd, 1900From a letter written to his father, announcing his intention to make"some experiments with a flying machine" at Kitty Hawk, North Carolina.

Numbering sequence: left to right, top to bottomPeople

A. U.S. World War I Aviator D. NASA Shuttle AstronautB. U.S. World War II Flier E. Space WalkersC. NASA Research PilotPlanetsI Saturn III Mars

6. Curtiss 1911 Model D7. Douglas World Cruiser (DWC) (formation)8. Ryan NYP "Spirit of St. Louis"9. North American P-51D Mustang (formation)

10. Boeing B-17 Flying Fortress11. Douglas SBD Dauntless (formation)12. Boeing Model 314 Clipper13. Consolidated PBY Catalina14. Boeing B-29 Superfortress

(Navy P2B-1S)/Douglas D-558-2 Skyrocket (launch)15. Douglas DC-3

22. Boeing 77723. Lockheed F-117 Nighthaw24. Rutan Model 76 Voyager25. Grumman F-14 Tomcat (fo26. Bell UH-1 Iroquois (Huey27. Apollo Spacecraft/Saturn V28. Grumman Lunar Module (29. Rockwell Shuttle (Space T

System)30. International Space Station31 Rockwell Space Shuttle Or


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SR-71/LASRE Configur ationNote:All dimensions in f eet

17.32


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2.50

107.40

41.21

Model7.1.86 Canoe

Reflector plane

2.75

55.60


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U S

A

U n i t e d S t a t e s


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S

A


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Ball nose config.

U S AIR F O

R C E


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U .S . A


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NA CA


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Lifting Body launchedfrom B-52

Maximum missionaltitude attained;

rocket engine shutdown


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Time

Altitude

B-52 with Lifting Bodyattached to pylon under wing

Unpowereglide to l

land

St k fl

Canard

Wing flap

27 ft 2.44 in.


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Strake flap

48 ft 1 in.

F-5A nosesection

Rudder


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Normal Bell-Nozzle

Rocket Engine

Linear Aerospike

Rocket Engine


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27.7 ft


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The supersonic airflow intothe engine is compressed

X - 43


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Co nven tional

Jet Engine

Scramjet EngineSupersonic combustion ramjets, or Scramjets,operate by burning fuel in a stream ofsupersonic air compressed by theforward speed of the aircraft.Unlike conventional jet engines,scramjets have no rotating parts.In normal jet engines, rotatingblades compress the air,and the airflow remainssub-sonic.

the engine is compressed

more as it enters the inletand passes through theengine. This increases theair pressure higher thanthe surrounding air.

Hydrogen fuel is ignitedin the supersonic airflow,with the rapid expansionof hot air out the exhaustnozzle producing thrust.

Rotating compressor blades draw in air and compress it.Mixture of fuel and air burns and expands in combustion chamber.


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12 ft


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Hyper-X

Pegasus b


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Interstage adapter


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