Experimental Roll-Damping, Magnus, and Static-Stability Characteristics of Two Slender Missile Configurations at High Angles of Attack (0 to 90 deg) and Mach Numbers 0.2 through 2.5

Mapping Intimacies ◽

10.21236/ada027027 ◽

1976 ◽

Cited By ~ 19

Author(s):

Leroy M. Jenke

Keyword(s):

Static Stability ◽

Roll Damping ◽

Mach Numbers ◽

High Angles Of Attack

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INVESTIGATION OF STATIC STABILITY AND AERODYNAMIC EFFECTS OF CONTROL JETS ON A 1/3-SCALE PYE WACKET MISSILE AT TRANSONIC MACH NUMBERS

10.21236/ad0320438 ◽

1960 ◽

Author(s):

D. C. BAKER ◽

L. L. GALIGHER

Keyword(s):

Static Stability ◽

Mach Numbers

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INVESTIGATION OF STING SUPPORT INTERFERENCE EFFECTS ON THE DYNAMIC AND STATIC STABILITY CHARACTERISTICS OF A 10-DEG CONE AT MACH NUMBERS 2.5, 3.0, AND 4.0,

10.21236/ad0450660 ◽

1964 ◽

Author(s):

B. L. Uselton

Keyword(s):

Static Stability ◽

Interference Effects ◽

Mach Numbers ◽

Support Interference

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Static Stability Wind-Tunnel Test of 18, 22, and 26 Caliber Cylinder- Ogive Bodies and an Aeroballistic Test Vehicle at Mach Numbers from 0.69 to 4. 24

10.21236/ad0775892 ◽

1953 ◽

Author(s):

Harvey Chaplin

Keyword(s):

Wind Tunnel ◽

Wind Tunnel Test ◽

Static Stability ◽

Test Vehicle ◽

Mach Numbers

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Experimental Static Stability Studies of Several Tactical Missile Configurations at Mach Numbers from 1.76 to 3.01

10.21236/ada009137 ◽

1975 ◽

Author(s):

E. Earl Lindsay ◽

J. L. Jordan

Keyword(s):

Static Stability ◽

Stability Studies ◽

Mach Numbers

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Static Stability and Drag Effects of Various External Store Configurations on the F-15 Aircraft at Mach Numbers from 0.6 to 1.3

10.21236/ada038494 ◽

1977 ◽

Author(s):

James M. Whoric

Keyword(s):

Static Stability ◽

Mach Numbers

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Experimental Results from a Static Stability and Pressure Test of the Minuteman Instrumented Payload Delivery System Launch Vehicle Configuration at Mach Numbers from 1.6 to 5.0

10.21236/adb014423 ◽

1976 ◽

Author(s):

E. E. Lindsay ◽

D. H. Fikes

Keyword(s):

Delivery System ◽

Static Stability ◽

Launch Vehicle ◽

Experimental Results ◽

Pressure Test ◽

Mach Numbers ◽

Vehicle Configuration

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Calibration of static pressure sensors using Extended Kalman Filter at high angles of attack and transonic Mach numbers

2016 Indian Control Conference (ICC) ◽

10.1109/indiancc.2016.7441170 ◽

2016 ◽

Cited By ~ 6

Author(s):

C Kamali ◽

Shikha Jain ◽

Amitabh Saraf ◽

Anup Goyal

Keyword(s):

Kalman Filter ◽

Extended Kalman Filter ◽

Static Pressure ◽

Pressure Sensors ◽

Mach Numbers ◽

High Angles Of Attack

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Investigation of the handling qualities of fighter aircraft with relaxed static stability at high angles of attack using a holistic simulation approach

International Conference on Simulation (1998) ◽

10.1049/cp:19980616 ◽

1998 ◽

Author(s):

L.D. Evangelou

Keyword(s):

Static Stability ◽

Simulation Approach ◽

Fighter Aircraft ◽

Handling Qualities ◽

High Angles Of Attack

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STATIC STABILITY CHARACTERISTICS OF A WINGED BODY WITH VARIOUS INLET CONFIGURATIONS AT MACH NUMBERS OF 2, 5, 8, AND 10

10.21236/ad0355573 ◽

1964 ◽

Author(s):

R. H. Burt ◽

M. E. Hillsamer

Keyword(s):

Static Stability ◽

Mach Numbers

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THE AERODYNAMIC CHARACTERISTICS OF A 75-DEG SWEPT DELTA WING AT HIGH ANGLES OF ATTACK AND MACH NUMBERS OF 2 TO 8 (U)

10.21236/ad0329345 ◽

1962 ◽

Author(s):

E. L. CLARK ◽

C. J. SPURLIN

Keyword(s):

Delta Wing ◽

Aerodynamic Characteristics ◽

Mach Numbers ◽

High Angles Of Attack

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