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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 55 records · Page 3

All sources NASA NTRS DOE OSTI

NASA NTRS1959

Low-Speed Investigation Of The Effects Of Horizontal-Tail Area And Wing Sweep On The Static Longitudinal Stability And Control Characteristics Of An Airplane Configuration Having Tail Surfaces Outboard Of The Wing Tips

Low-speed longitudinal static stability & control characteristics of aircraft with swept wings & tail surfaces outboard of wing tips

STABILITY AND CONTROL↗

NASA NTRS1959

Flutter Investigation at a Mach Number of 7.2 of Models of the Horizontal-tail and Vertical-tail Surfaces of the X-15 Airplane

Flutter studies at Mach 7.2 of horizontal and vertical tail surface models of X-15 aircraft

TAIL SURFACE↗

NASA NTRS1945

Investigation of Effect of Sideslip on Lateral Stability Characteristics III : Rectangular Low Wing on Circular Fuselage with Variations in Vertical-tail Area and Fuselage Length With and Without Horizontal Tail Surface

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MONOPLANES, LOW-WING↗

NASA NTRS1948

Measurements of the Pressure Distribution on the Horizontal-tail Surface of a Typical Propeller-driven Pursuit Airplane in Flight III : Tail Loads in Abrupt Pull-up Push-down Maneuvers

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LOADS - TAIL SURFACES, HORIZONTAL↗

NASA NTRS1950

Effect of Horizontal Tail on Low-speed Static Lateral Stability Characteristics of a Model Having 45 Degree Sweptback Wing and Tail Surfaces

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WINGS, SWEPTBACK - CHARACTERISTICS↗

NASA NTRS1945

Investigation of Effect of Sideslip on Lateral Stability Characteristics II : Rectangular Midwing on Circular Fuselage with Variations in Vertical-tail Area and Fuselage Length with and Without Horizontal Tail Surface

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TAIL SURFACES, HORIZONTAL↗

NASA NTRS1945

Experimental verification of a simplified vee-tail theory and analysis of available data on complete models with vee tails

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TAIL SURFACES, VEE↗

NASA NTRS1944

Estimates of the Vertical-Tail Loads of a Bell P-63A-1 Airplane (AAF No. 42-68889) in Accelerated Rolling Maneuvers Based on Flight Tests with Two Vertical-Tail Arrangements

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TAIL SURFACES, VERTICAL - BELL P-63A-1 - FLIGHT TE↗

NASA NTRS1948

The Effect of Variations in Moments of Inertia on Spin and Recovery Characteristics of a Single-Engine Low-wing Monoplane with Various Tail Arrangements, Including a Twin Tail

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SPINNING TESTS - MONOPLANES - WIND TUNNEL (NACA-FR↗

NASA NTRS1943

Flight Tests of Various Tail Modifications on the Brewster XSBA-1 Airplane I : Measurements of Flying Qualities with Original Tail Surfaces

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AIRPLANES - BREWSTER SBA-1 FLIGHT TESTS (EXPERIMEN↗

NASA NTRS1944

Flight Tests of Various Tail Modifications on the Brewster XSBA-1 Airplane III : Measurements of Flying Qualities with Tail Configuration 3

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AIRPLANES - FLYING QUALITIES↗

NASA NTRS1950

Wind-Tunnel Investigation of a 0.6-Scale Model of Hughes MX-904 Tail Surface at Supersonic Speeds. Tail Attached to a Segment of the Foreshortened Body

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Conner, D. W.↗

NASA NTRS1979

Pressure distributions on three different cruciform aft-tail control surfaces of a wingless missile at Mach 1.60, 2.36, and 3.70. Volume 3: Cranked tail

The results of pressure distribution tests are presented without analysis. The test Reynolds number used was 6.6. x 10 to the 6th power per meter.

Lamb, M.↗

NASA NTRS1941

The end-plate effect of a horizontal-tail surface on vertical tail surface

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KATZOFF S↗

NASA NTRS1950

Experimental Investigation of the Effect of Vertical-tail Size and Length of Fuselage Shape and Length on the Static Lateral Stability Characteristics of a Model with 45 Degree Sweptback Wing and Tail Surfaces

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Queijo, M J↗

NASA NTRS1953

Effect of horizontal-tail span and vertical location on the aerodynamic characteristics of an unswept tail assembly in sideslip

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Riley, Donald R↗

NASA NTRS1954

Some Effects of Aspect Ratio and Tail Length on the Contribution of a Vertical Tail to Unsteady Lateral Damping and Directional Stability of a Model Oscillating Continuously in Yaw

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Fisher, Lewis R↗

NASA NTRS1949

Investigation of the dynamic lateral stability and control characteristics of a model of a fighter airplane without a horizontal tail and equipped with either single or twin vertical tails

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Draper, John W↗