Effect of several tail configurations on the stability characteristics of a midwing supersonic-bomber model at mach numbers of 1.60, 1.90, 2.20, and 2.50 / | ORKG Ask

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Langley Research Center.

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Lateral directional stability characteristics at mach 2.3 to 3.5 of a supersonic transport model with various outboard vertical-tail locations /

Corlett, William A.
Langley Research Center.

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Langley Research Center.
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Leavitt, Laurence D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

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Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds /

Blair, A. B.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Dec. 1980."Langley Research Center."Includes bibliographical references.Mode of access: Internet

Experimental and theoretical supersonic lateral-directional stability characteristics of a simplified wing-body configuration with a series of vertical-tail arrangements /

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Thomas, James L. (James Lee), 1952-
Sawyer, Wallace C.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"August 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: I...

Stability and control characteristics of a monoplanar missile configuration with triform-tail-fin arrangements at mach numbers from 1.70 to 2.86 /

Lamb, Milton.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

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Stability and control characteristics of a three-surface advanced fighter configuration at angles of attack up to 45?/

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Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

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Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds /

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Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

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