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Investigation of Lateral Stability at Stall
Language: en
Pages: 136

Investigation of Lateral Stability at Stall

Authors: Gifford Bull
Categories: Stability of airplanes, Lateral
Type: BOOK - Published: 1954 - Publisher:

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Investigation of Lateral Stability at Stall
Language: en
Pages: 1

Investigation of Lateral Stability at Stall

Authors: CORNELL AERONAUTICAL LAB INC BUFFALO NY.
Categories:
Type: BOOK - Published: 1954 - Publisher:

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Simulator Study of Stall/post-stall Characteristics of a Fighter Airplane with Relaxed Longitudinal Static Stability
Language: en
Pages: 236

Simulator Study of Stall/post-stall Characteristics of a Fighter Airplane with Relaxed Longitudinal Static Stability

Authors:
Categories:
Type: BOOK - Published: 1979 - Publisher:

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Longitudinal-stability Investigation of High-lift and Stall-control Devices on a 52 Degrees Sweptback Wing with and Without Fuselage and Horizontal Tail at a Reynolds Number of 6.8 X (10)6
Language: en
Pages: 41

Longitudinal-stability Investigation of High-lift and Stall-control Devices on a 52 Degrees Sweptback Wing with and Without Fuselage and Horizontal Tail at a Reynolds Number of 6.8 X (10)6

Authors: Gerald V. Foster
Categories:
Type: BOOK - Published: 1948 - Publisher:

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Investigation of the Variation of Maximum Lift for a Pitching Airplane Model and Comparison with Flight Results
Language: en
Pages: 704

Investigation of the Variation of Maximum Lift for a Pitching Airplane Model and Comparison with Flight Results

Authors: Paul W. Harper
Categories: Airplanes
Type: BOOK - Published: 1948 - Publisher:

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Apparatus was developed which utilized a pitching airplane model to determine maximum wing loads as a function of the rate of change of angle of attack. In orde