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1
An Investigation of Aircraft Heaters XXXVII : Experimental Determination of Thermal and Hydrodynamical Behavior of Air Flowing Along a Flat Plate Containing Turbulence Promotors
An Investigation of Aircraft Heaters XXXVII : Experimental Determination of Thermal and Hydrodynamical Behavior of Air Flowing Along a Flat Plate Containing Turbulence Promotors
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An Investigation of Aircraft Heaters XXXVII : Experimental Determination of Thermal and Hydrodynamical Behavior of Air Flowing Along a Flat Plate Containing Turbulence Promotors

Boetler, L M K ; Young, G ; Greenfield, M L ; Sanders, V D ; Morgan, M

Legacy CDMS 1951

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2
An Investigation of Aircraft Heaters. 37. Experimental Determination of Thermal and Hydrodynamical Behavior of Air Flowing Along a Flat Plate Containing Turbulence Promoters
An Investigation of Aircraft Heaters. 37. Experimental Determination of Thermal and Hydrodynamical Behavior of Air Flowing Along a Flat Plate Containing Turbulence Promoters
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An Investigation of Aircraft Heaters. 37. Experimental Determination of Thermal and Hydrodynamical Behavior of Air Flowing Along a Flat Plate Containing Turbulence Promoters

Boelter, L M ; Young, G ; Greenfield, M L ; Sanders, V D ; Morgan, M

1951

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3
An Investigation of Aircraft Heaters XXXIV-Experimental Determination of Thermal And Hydrodynamical Behavior of Air Flowing Between a Flat and a Wave-Shaped Plate
An Investigation of Aircraft Heaters XXXIV-Experimental Determination of Thermal And Hydrodynamical Behavior of Air Flowing Between a Flat and a Wave-Shaped Plate
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An Investigation of Aircraft Heaters XXXIV-Experimental Determination of Thermal And Hydrodynamical Behavior of Air Flowing Between a Flat and a Wave-Shaped Plate

Boelter, L M ; Sanders, V D ; Young, G ; Morgan, M ; Morrin, E H

1951

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4
An investigation of aircraft heaters XXXIV : experimental determination of thermal and hydrodynamical behavior of air flowing between a flat and a wave-shaped plate
An investigation of aircraft heaters XXXIV : experimental determination of thermal and hydrodynamical behavior of air flowing between a flat and a wave-shaped plate
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An investigation of aircraft heaters XXXIV : experimental determination of thermal and hydrodynamical behavior of air flowing between a flat and a wave-shaped plate

Boelter, Llewellyn Michael Kraus ; Sanders, V D ; Young, George ; Morgan, M ; Morrin, E H

Legacy CDMS 1951

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5
AQUEOUS CHROMIUM (III) SULFATE SOLUTIONS. I. CHEMICAL PROPERTIES OF AGED SOLUTIONS
AQUEOUS CHROMIUM (III) SULFATE SOLUTIONS. I. CHEMICAL PROPERTIES OF AGED SOLUTIONS
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AQUEOUS CHROMIUM (III) SULFATE SOLUTIONS. I. CHEMICAL PROPERTIES OF AGED SOLUTIONS

MORGAN,L.O ; MUTCHLER,JEAN M ; GIPSON,JEFFREY

1955

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6
Transonic wind-tunnel investigation of the effects of taper ratio, body indentation, fixed transition, and afterbody shape on the aerodynamic characteristics of a 45 degree sweptback wing-body combination
Transonic wind-tunnel investigation of the effects of taper ratio, body indentation, fixed transition, and afterbody shape on the aerodynamic characteristics of a 45 degree sweptback wing-body combination
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Transonic wind-tunnel investigation of the effects of taper ratio, body indentation, fixed transition, and afterbody shape on the aerodynamic characteristics of a 45 degree sweptback wing-body combination

Morgan, Francis G, Jr ; Carmel, Melvin M

Legacy CDMS 1954

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7
Investigation of a High-pressure-ratio Eight-stage Axial-flow Research Compressor with Two Transonic Inlet Stages VI : Over-all Performance, Rotating Stall, and Blade Vibration at Low and Intermediate Compressor Speeds
Investigation of a High-pressure-ratio Eight-stage Axial-flow Research Compressor with Two Transonic Inlet Stages VI : Over-all Performance, Rotating Stall, and Blade Vibration at Low and Intermediate Compressor Speeds
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Investigation of a High-pressure-ratio Eight-stage Axial-flow Research Compressor with Two Transonic Inlet Stages VI : Over-all Performance, Rotating Stall, and Blade Vibration at Low and Intermediate Compressor Speeds

Standahar, Raymond M ; Hanson, Morgan P ; Geye, Richard P

Legacy CDMS 1955

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8
An Investigation of the Stream-tube Power Losses and an Improvement of the Diffuser-entrance Nose in the Langley 8-foot Transonic Tunnel
An Investigation of the Stream-tube Power Losses and an Improvement of the Diffuser-entrance Nose in the Langley 8-foot Transonic Tunnel
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An Investigation of the Stream-tube Power Losses and an Improvement of the Diffuser-entrance Nose in the Langley 8-foot Transonic Tunnel

Whitcomb, Richard T ; Carmel, Melvin M ; Morgan, Francis G, Jr

Legacy CDMS 1952

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9
Effect of Compressibility and Camber as Determined from an Investigation of the NACA 4-(3)(08)-03 and 4-(5)(08)-03 Two-blade Propellers up to Forward Mach Numbers of 0.925
Effect of Compressibility and Camber as Determined from an Investigation of the NACA 4-(3)(08)-03 and 4-(5)(08)-03 Two-blade Propellers up to Forward Mach Numbers of 0.925
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Effect of Compressibility and Camber as Determined from an Investigation of the NACA 4-(3)(08)-03 and 4-(5)(08)-03 Two-blade Propellers up to Forward Mach Numbers of 0.925

Carmel, Melvin M ; Morgan, Francis G, Jr ; Coppolino, Domenic A

Legacy CDMS 1950

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10
Flight Investigation of the Cooling Characteristics of a Two-row Radial Engine Installation III : Engine Temperature Distribution
Flight Investigation of the Cooling Characteristics of a Two-row Radial Engine Installation III : Engine Temperature Distribution
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Flight Investigation of the Cooling Characteristics of a Two-row Radial Engine Installation III : Engine Temperature Distribution

Rennak, Robert M ; Messing, Wesley E ; Morgan, James E

Legacy CDMS 1946

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