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The Effects of Static Margin and Rotational Damping in Pitch on the Longitudinal Stability Characteristics of an Airplane as Determined by Tests of a Model in the NACA Free-flight Tunnel
Language: en
Pages: 26

The Effects of Static Margin and Rotational Damping in Pitch on the Longitudinal Stability Characteristics of an Airplane as Determined by Tests of a Model in the NACA Free-flight Tunnel

Authors: John P. Campbell
Categories: Aerodynamics
Type: BOOK - Published: 1944 - Publisher:

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Summary: The effects of static margin and rotational damping in pitch on the longitudinal stability characteristics of an airplane have been determined by fligh
The Effects of Static Margin and Rotational Damping in Pitch on the Longitudinal Stability Characteristics of an Airplane as Determined by Tests of a Model in the N.A.C.A. Free-flight Tunnel
Language: en
Pages:

The Effects of Static Margin and Rotational Damping in Pitch on the Longitudinal Stability Characteristics of an Airplane as Determined by Tests of a Model in the N.A.C.A. Free-flight Tunnel

Authors: John P. Campbell
Categories:
Type: BOOK - Published: 1945 - Publisher:

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Effects of Static Margin and Rotational Damping in Pitch on the Longitudinal Stability Characteristics of an Airplane as Determined by Tests of a Model in the NACA Free-flight Tunnel
Language: en
Pages: 26

Effects of Static Margin and Rotational Damping in Pitch on the Longitudinal Stability Characteristics of an Airplane as Determined by Tests of a Model in the NACA Free-flight Tunnel

Authors: Langley Aeronautical Laboratory
Categories:
Type: BOOK - Published: 2021-09-09 - Publisher: Hassell Street Press

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This work has been selected by scholars as being culturally important and is part of the knowledge base of civilization as we know it. This work is in the publi
The Effects of Static Margin and Rotational Damping in Pitch on the Longitudinal Stability Characteristics of an Airplane as Determined by Tests of a Model in the NACA.
Language: en
Pages: 20

The Effects of Static Margin and Rotational Damping in Pitch on the Longitudinal Stability Characteristics of an Airplane as Determined by Tests of a Model in the NACA.

Authors:
Categories:
Type: BOOK - Published: 1944 - Publisher:

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Report - National Advisory Committee for Aeronautics
Language: en
Pages: 586

Report - National Advisory Committee for Aeronautics

Authors: United States. National Advisory Committee for Aeronautics
Categories: Aeronautics
Type: BOOK - Published: 1944 - Publisher:

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