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Results for “Camber”

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 253 records · Page 14

All sources NASA NTRS DOE OSTI

NASA NTRS1954

A Transonic Wind-tunnel Investigation of the Longitudinal Force and Moment Characteristics of a Plane and a Cambered 3-percent-thick Delta Wing of Aspect Ratio 3 on a Slender Body

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Burrows, Dale L↗

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

A transonic wind-tunnel investigation of the static longitudinal characteristics of a 3-percent-thick, aspect-ratio-3, delta wing cambered and twisted for high lift-drag ratios

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Burrows, Dale L↗

NASA NTRS1955

Effects of leading-edge radius on the longitudinal stability of two 45 degree sweptback wings incorporating leading edge camber as influenced by Reynolds numbers up to 8.00 x 10(exp 6) and Mach numbers up to 0.29

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Foster, Gerald V↗

NASA NTRS1956

Effect of Wing Camber and Twist at Mach Numbers from 1.4 to 2.1 on the Lift, Drag, and Longitudinal Stability of a Rocket-powered Model Having a 52.5 Degree Sweptback Wing of Aspect Ratio 3 and Inline Tail Surfaces

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Gillespie, Warren, Jr↗

NASA NTRS1956

Low-speed stability characteristics of a cambered-delta-wing model

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Riebe, John M↗

NASA NTRS1956

Investigation of the Effects of Body Camber and Body Indentation on the Longitudinal Characteristics of a 60 Degree Delta-wing--body Combination at a Mach Number of 1.61

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Sevier, John R , Jr↗

NASA NTRS1956

Effect of Blade-section Camber on Aerodynamic Characteristics of Full-scale Supersonic-type Propellers at Mach Numbers to 1.04

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Maynard, Julian D↗

NASA NTRS1956

Effect of camber on the drag of a body of revolution

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Dickey, Robert R↗

NASA NTRS1956

Pressure distributions at Mach numbers of 1.6 and 1.9 of a conically cambered wing of triangular plan form with and without pylon-mounted engine nacelles

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Phelps, E Ray↗

NASA NTRS1956

Static Stability Characteristics of a Cambered-delta-wing Model at High Subsonic Speeds

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Moseley, William C , Jr↗

NASA NTRS1957

Investigation at Mach Numbers to 1.04 of Blade-loading Characteristics of Two Full-scale Three-blade Supersonic Propellers Differing in Blade-section Camber

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Salters, Leland B , Jr↗

NASA NTRS1957

Transonic flutter characteristics of a cambered A-plan-form wing with and without simulated nacelles

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Kelly, H Neale↗

NASA NTRS1957

Pressure measurements at transonic and low supersonic speeds on a thin conical cambered low-aspect-ratio delta wing in combination with basic and indented bodies

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Mugler, John P JR↗

NASA NTRS1957

Effects of conical camber on the lift, drag, and pitching-moment characteristics of a triangular wing of aspect ratio 3.0

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Peterson, Victor, L↗

NASA NTRS1957

Low-speed cascade investigation of thin low-camber NACA 65-series blade sections at high inlet angles

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Emery, James C↗

NASA NTRS1958

The Static Longitudinal Characteristics of a Twisted and Cambered 45 Degree Sweptback Wing at Mach Numbers up to 0.96

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Sammonds, Robert I↗

NASA NTRS1958

Aerodynamic Characteristics at Mach Numbers 2.36 and 2.87 of an Airplane Configuration Having a Cambered Arrow Wing with a 75 Degree Swept Leading Edge

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Hallissy, Joseph M , Jr↗