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Results for “STABILITY, LONGITUDINAL - DYNAMIC”

Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.

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At least 199 records · Page 11

All sources NASA NTRS DOE OSTI

NASA NTRS1948

Longitudinal Stability and Control Characteristics of a Semispan Airplane Model with a Sweptback Wing and Tail from Tests at Transonic Speeds by the NACA Wing-flow Method

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Sawyer, Richard H↗

NASA NTRS1948

High-speed Wind-tunnel Tests of a 1/16-scale Model of the D-558 Research Airplane Longitudinal Stability and Control of the D-558-1

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Wright, John B↗

NASA NTRS1948

Determination by the free-fall method of the longitudinal stability and control characteristics of a 1/4-scale model of the Bell XS-1 airplane at transonic speeds

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Matthews, James T↗

NASA NTRS1948

Longitudinal Stability and Control Characteristics of a Semispan Model of a Supersonic Airplane Configuration at Transonic Speeds from Tests by the NACA Wing-flow Method

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Silsby, Norman S↗

NASA NTRS1948

Longitudinal Stability and Control Characteristics of a Semispan Airplane Model at Transonic Speeds as Obtained by the Transonic-bump Method

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Weil, Joseph↗

NASA NTRS1947

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↗

NASA NTRS1948

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↗

NASA NTRS1948

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↗

NASA NTRS1949

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↗

NASA NTRS1949

High Speed Wind-Tunnel Investigation of the Longitudinal Stability and Control Characteristics of a 1/16-Scale Model of the D-558-2 Research Airplane at High Subsonic Mach Number and at a Mach Number of 1.2

No abstract available

Osborne, Robert S↗

NASA NTRS1949

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↗

NASA NTRS1949

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↗

NASA NTRS1949

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↗

NASA NTRS1950

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↗

NASA NTRS1949

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↗

NASA NTRS1949

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↗

NASA NTRS1949

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↗

NASA NTRS1949

Some tests of the longitudinal stability and control of an H-13B helicopter in forward flight

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Reeder, John P↗