Longitudinal Stability and Control Characteristics of a Semispan Airplane Model with a Swept-back Tail from Tests at Transonic Speeds by the NACA Wing-flow Method
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Zalovcik, John A↗
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Results for “LONGITUDINAL STABILITY”
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Flight-test Evaluation of the Longitudinal Stability and Control Characteristics of 0.5-scale Models of the Lark Pilotless-aircraft Configuration
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Stone, David G↗
High-speed Wind-tunnel Tests of a 1/16-scale Model of the D-558 Research Airplane Basic Longitudinal Stability of the D-558-1
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Wright, John B↗
Longitudinal Stability and Control Characteristics of a Semispan Wind-tunnel Model of a Tailless Airplane and a Comparison with Complete-model Wind-tunnel Tests and Semispan-model Wing-flow Tests
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Goodson, Kenneth W↗
Static Longitudinal Stability and Control of a Convertible-type Airplane as Affected by Articulated- and Rigid-propeller Operation
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Lange, Roy H↗
The Effect of Span and Deflection of Split Flaps and Leading-edge Roughness on the Longitudinal Stability and Gliding Characteristics of a 42 Degree Sweptback Wing Equipped with Leading-edge Flaps
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Pratt, George L↗
Low-speed static longitudinal stability characteristics of a canard model having a 60 degrees triangular wing and horizontal tail
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Bates, William R↗
Maximum lift and longitudinal stability characteristics at Reynolds numbers up to 7.8 x 10(exp 6) of a 35 degree sweptforward wing equipped with high-lift and stall-control devices, fuselage, and horizontal tail
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Martina, Albert P↗
Low-speed Wind-tunnel Investigation of the Longitudinal Stability Characteristics of a Model Equipped with a Variable-sweep Wing
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Donlan, Charles J↗
Preliminary flight measurements of the static longitudinal stability and stalling characteristics of the Douglas D-558-II research airplane (BuAero No. 37974)
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Sjoberg, S A↗
Investigation of a Thin Wing of Aspect Ratio 4 in the Ames 12-foot Pressure Wind Tunnel V : Static Longitudinal Stability and Control Throughout the Subsonic Speed Range of a Semispan Model of a Supersonic Airplane
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Johnson, Ben H , Jr↗
Some tests of the longitudinal stability and control of an H-13B helicopter in forward flight
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Reeder, John P↗
Preliminary results from a free-flight investigation at transonic and supersonic speeds of the longitudinal stability and control characteristics of an airplane configuration with a thin straight wing of aspect ratio 3
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Gillis, Clarence L↗
Determination by the Free-fall Method of the Drag and Longitudinal Stability and Control Characteristics of a Canard Model at Transonic Speeds
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Kraft, Christopher C , Jr↗
An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular-arc Sections and 40 Degree Sweepback : Static Longitudinal Stability and Control Characteristics at a Mach Number of 1.59
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Spearman, M Leroy↗
Longitudinal Stability and Control Characteristics at High Subsonic Speeds of Two Models of a Transonic Research Airplane with Wings and Horizontal Tails of Aspect Ratios 4.2 and 2
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Luoma, Arvo A↗
Wing-flow Measurements of Longitudinal Stability and Control Characteristics of a Supersonic Airplane Configuration Having a 42.8 Degree Sweptback Circular Arc Wing with Aspect Ratio 4.0, Taper Ratio 0.50, and Sweptback Tail Surfaces
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Crane, Harold L↗