Engineering topics

Strass, H Kurt

Publications and source records attributed to Strass, H Kurt.

At least 19 records

All sources NASA NTRS DOE OSTI

NASA NTRS1958

Some Effects of Roughness on Stagnation-point Heat Transfer at a Mach Number of 2, a Stagnation Temperature of 3,530 Degrees F, and a Reynolds Number of 2.5 x 10(exp 6) Per Foot

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Strass, H Kurt↗

NASA NTRS1957

Aerodynamic Heating of a Thin, Unswept, Untapered, Multiweb, Aluminum-alloy Wing at Mach Numbers up to 2.67 as Determined from a Free-flight Investigation of a Rocket-propelled Model

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Strass, H Kurt↗

NASA NTRS1957

Two factors influencing temperature distributions and thermal stresses in structures

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Brooks, William A , Jr↗

NASA NTRS1955

Collection and Summary of Flap-type-aileron Rolling-effectiveness Data at Zero Lift as Determined by Rocket-powered Model Tests at Mach Numbers Between 0.6 and 1.6

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Strass, H Kurt↗

NASA NTRS1954

Some Effects of Aileron Span, Aileron Chord, and Wing Twist on Rolling Effectiveness as Determined by Rocket-powered Model Tests and Theoretical Estimates

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Strass, H Kurt↗

NASA NTRS1954

Summary of Some Rocket-model Investigations of Effects of Wing Aspect Ratio and Thickness on Aileron Rolling Effectiveness Including Some Effects of Spanwise Aileron Location for Sweptback Wings with Aspect Ratio of 8.0

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Strass, H Kurt↗

NASA NTRS1953

An engineering method for the determination of aeroelastic effects upon the rolling effectiveness of ailerons on swept wings

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Strass, H Kurt↗

NASA NTRS1953

Investigations toward simplification of missile control systems

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Curfman, Howard J , Jr↗

NASA NTRS1953

Recent Experiences with Flutter Failure of Sweptback, Tapered Wings Having Outboard, Partial-span Spoiler Controls

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Strass, H Kurt↗

NASA NTRS1952

Rocket-model Investigation of the Rolling Effectiveness of a Fighter-type Wing-control Configuration at Mach Numbers from 0.6 to 1.5

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Strass, H Kurt↗

NASA NTRS1952

Free-flight Measurements of Some Effects of Aileron Span, Chord, and Deflection and of Wing Flexibility on the Rolling Effectiveness of Ailerons on Sweptback Wings at Mach Numbers Between 0.8 and 1.6

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Strass, H Kurt↗

NASA NTRS1952

Summary of Some Effective Aerodynamic Twisting-moment Coefficients of Various Wing-control Configurations at Mach Numbers from 0.6 to 1.7 as Determined from Rocket-powered Models

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Strass, H Kurt↗

NASA NTRS1951

Rolling Effectiveness of All-movable Wings at Small Angles of Incidence at Mach Numbers from 0.6 to 1.6

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Strass, H Kurt↗

NASA NTRS1951

Free-flight Measurements at Mach Numbers from 0.7 to 1.6 of Some Effects of Airfoil-thickness Distribution and Trailing-edge Angle on Aileron Rolling Effectiveness and Drag for Wings with 0 and 45 Degrees Sweepback

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Fields, E M↗

NASA NTRS1951

Some effects of spanwise aileron location and wing structural rigidity on the rolling effectiveness of 0.3-chord flap-type ailerons on a tapered wing having 63 degrees sweepback at the leading edge and NACA 64A005 airfoil sections

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Strass, H Kurt↗

NASA NTRS1950

Experimental determination of effect of structural rigidity on rolling effectiveness of some straight and swept wings at Mach numbers from 0.7 to 1.7

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Strass, H Kurt↗

NASA NTRS1950

The Rolling Effectiveness of Wing-tip Ailerons as Determined by Rocket-powered Test Vehicles and Linear Supersonic Theory

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Sandahl, Carl A↗

NASA NTRS1950

Rolling Effectiveness of a Thin Tapered Wing Having Partial-span Ailerons as Determined by Rocket-powered Test Vehicles

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Sandahl, Carl A↗