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* C A n particle/m 3 C l S m 2 C m V m/s C mq x, y, z C n α C N β C p λ C Y ¯ d m hs D m T Kn cg M b * 43rd AIAA Aerospace Sciences Meeting and Exhibit 10 - 13 January 2005, Reno, Nevada AIAA 2005-56 This material is declared a work of the U.S. Government and is not subject to copyright protection in the United States.

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Page 1: [American Institute of Aeronautics and Astronautics 43rd AIAA Aerospace Sciences Meeting and Exhibit - Reno, Nevada ()] 43rd AIAA Aerospace Sciences Meeting and Exhibit - Static Aerodynamics

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43rd AIAA Aerospace Sciences Meeting and Exhibit10 - 13 January 2005, Reno, Nevada

AIAA 2005-56

This material is declared a work of the U.S. Government and is not subject to copyright protection in the United States.

Page 2: [American Institute of Aeronautics and Astronautics 43rd AIAA Aerospace Sciences Meeting and Exhibit - Reno, Nevada ()] 43rd AIAA Aerospace Sciences Meeting and Exhibit - Static Aerodynamics

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Page 3: [American Institute of Aeronautics and Astronautics 43rd AIAA Aerospace Sciences Meeting and Exhibit - Reno, Nevada ()] 43rd AIAA Aerospace Sciences Meeting and Exhibit - Static Aerodynamics

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Page 4: [American Institute of Aeronautics and Astronautics 43rd AIAA Aerospace Sciences Meeting and Exhibit - Reno, Nevada ()] 43rd AIAA Aerospace Sciences Meeting and Exhibit - Static Aerodynamics

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ds

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�v� λ/ds �v� λ/ds �v� λ/ds �v� λ/ds �v� λ/ds

100 CO2 65 CO2 43 CO2 64 CO2 59 CO2 69

30 �vz� 19 CO2 17 CO2 18.5 CO2 17 CO2 17.3

10 �vz� 5.8 CO2 13.2 �vz� 13.8 CO2 5.3 CO2 13

3 �vz� 1.4 CO2 1.3 �vz� 1.4 CO2 1.3 CO2 1.3

1 �vz� 2.8 �vz� 1.3 �vz� 1.0 �vz� 0.4 �vz� 1.0

0.30 �vz� 0.9 �vz� 0.9 �vz� 0.8 �vz� 0.5 �vz� 0.5

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0.4 0.5 0.7 0.9 1.1 1.3 2.0 2.2 2.4 2.6 2.8 3.0 3.2 3.4 3.6 3.8 4.0 4.2 4.4 4.6 4.8 5.0 5.2 5.4 5.5

2.0 3.0 4.1 5.1 6.3 8.8 9.7 10.6 11.5 12.5 13.4 14.3 15.2 16.1 17.1 18.0 19.0 20.0 21.0 22.0 23.0 24.2 25.4 26.7

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4

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Mach

Velocity, km/s

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deg

LAURA Perfect Gas, Forebody + Base Correction

LAURA Nonequilibrium, Forebody Only

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a1

M∞

+a2

M2∞

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M3∞

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a0 = 8.325E−03

a1 = 1.129E−01

a2 = −1.801E−00

a3 = 1.288E−00 �¥ ��� � C köqnpö ol� D �ömqöö�il

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Kn

Cm

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0.01

0.02

0.03

0.04

0.05

0.06

0.07

0.08

0.09

0.10

0.11

0.12

0.13

0.14

20°

16°

10°

DAC, transitionalLAURA, continuumDACFREE, free molecular

20°

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Page 9: [American Institute of Aeronautics and Astronautics 43rd AIAA Aerospace Sciences Meeting and Exhibit - Reno, Nevada ()] 43rd AIAA Aerospace Sciences Meeting and Exhibit - Static Aerodynamics

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