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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 541 records · Page 30

All sources NASA NTRS DOE OSTI

NASA NTRS1955

A transonic wind-tunnel investigation of the longitudinal force and moment characteristics of two delta wings and one clipped-tip delta wing of 4 percent thickness on a slender body

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Palmer, William E↗

NASA NTRS1955

Comparison of the static stability of a 68.7 degree delta-wing model with dihedral and a twisted and cambered wing model of the same plan form

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Paulson, John W↗

NASA NTRS1955

Experimental Static Aerodynamic Forces and Moments at Low Speed on a Canard Missle During Simulated Launching from the Midsemispan and Wing-tip Locations of a 45 Degree Sweptback Wing-fuselage Combination

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Alford, William J , Jr↗

NASA NTRS1955

Experimental Investigation of Some Aerodynamic Effects of a Gap Between Wing and Body of a Moderately Slender Wing-body Combination at a Mach Number of 1.4

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Dugan, Duane W↗

NASA NTRS1955

Low-speed Investigation of the Effects of Wing Tanks and Speed Brakes on the Static Stability of a Model Having a 40 Degree Swept Wing

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Sleeman, William C , Jr↗

NASA NTRS1955

Flight Measurements of Wing Loads on the Convair XF-92A Delta-wing Airplane

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Kuhl, Albert E↗

NASA NTRS1955

The origin and distribution of supersonic store interference from measurement of individual forces on several wing-fuselage-store configurations I : swept-wing heavy-bomber configuration with large store (nacelle). lift and drag; Mach number, 1.61

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Smith, Norman F↗

NASA NTRS1955

Experimental Static Aerodynamic Forces and Moments at Low Speed on a Missile Model During Simulated Launching from the 25-percent-semispan and Wing-tip Locations of a 45 Degree Sweptback Wing-fuselage Combination

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Alford, William J , Jr↗

NASA NTRS1955

Load distributions on wings and wing-body combinations at high angles of attack and supersonic speeds

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Katzen, Elliott D↗

NASA NTRS1955

Investigation of the effects of body indentation and of wing-plan-form modification on the longitudinal characteristics of a 60 degree swept-wing-body combination at Mach numbers of 1.41, 1.61, and 2.10

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Sevier, John R , Jr↗

NASA NTRS1956

Effect of Wing Size and Amount of Indentation on Applicability of Transonic Area Rule to Swept-wing Configurations

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Hall, James Rudyard↗

NASA NTRS1955

Effects of taper ratio on the longitudinal characteristics at Mach numbers from 0.6 to 1.4 of a wing-body-tail combination having an unswept wing of aspect ratio 3

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Summers, James L↗

NASA NTRS1955

Wing Pressure Distributions over the Lift Range of the Convair XF-92A Delta-wing Airplane at Subsonic and Transonic Speeds

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Keeener, Earl R↗

NASA NTRS1956

Transonic Wind-tunnel Investigation of the Effects of Incidence and Body Indentation on the Wing Loads of a 45 Degree Sweptback Wing-body Combination

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Platt, Robert J , Jr↗

NASA NTRS1955

Flight measurements of the loads and moments on an external store mounted under the wing of a swept-wing fighter-type airplane during yawing and rolling maneuvers

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Hamer, Harold A↗

NASA NTRS1955

The origin and distribution of supersonic store interference from measurement of individual forces on several wing-fuselage-store configurations IV : delta-wing heavy-bomber configuration with large store. Mach number, 1.61

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Morris, Odell A↗

NASA NTRS1955

The Origin and Distribution of Supersonic Store Interference from Measurement of Individual Forces on Several Wing-fuselage-store Configurations III : Swept-wing Fighter-bomber Configuration with Large and Small Stores. Mach Number, 1.61

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Smith, Norman F↗

NASA NTRS1956

The Effect of Leading-edge Extensions on the Longitudinal Characteristics at Mach Numbers up to 0.92 of a Wing-fuselage-tail Combination Having a 40 Degree Sweptback Wing with NACA 64A Thickness Distribution

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Sutton, Fred B↗