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Refinado por: Base de dados/Biblioteca: Aerospace Database remover tipo de recurso: Reports remover
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1
Growth of a turbulent wake behind a supersonic sphere
Growth of a turbulent wake behind a supersonic sphere
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Growth of a turbulent wake behind a supersonic sphere

DICKINSON, E R M U R P H Y, C H

BALLISTIC RESEARCH LABS., ABERDEEN PROVING GROUND, MD. GROWTH OF THE TURBULENT WAKE BEHIND A SUPERSONIC SPHERE. CHARLES H. MURPHY AND ELIZABETH R. DICKINSON, 1962

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2
Large-scale wind-tunnel tests of descent performance of an airplane model with a tilt wing and differential propeller thrust (Wind tunnel tests of wing stall, performance, and longitudinal stability & control of large model v/stol tilt wing transport aircraft)
Large-scale wind-tunnel tests of descent performance of an airplane model with a tilt wing and differential propeller thrust (Wind tunnel tests of wing stall, performance, and longitudinal stability & control of large model v/stol tilt wing transport aircraft)
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Large-scale wind-tunnel tests of descent performance of an airplane model with a tilt wing and differential propeller thrust (Wind tunnel tests of wing stall, performance, and longitudinal stability & control of large model v/stol tilt wing transport aircraft)

Deckert, W H ; Dickinson, S O ; Page, V R

WASHINGTON, NASA, 1964, p.42 P-42 P

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3
Plasma electron beam welder for space vehicles Final report (Feasibility of developing plasma electron beam welding system for earth orbiting vehicle)
Plasma electron beam welder for space vehicles Final report (Feasibility of developing plasma electron beam welding system for earth orbiting vehicle)
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Plasma electron beam welder for space vehicles Final report (Feasibility of developing plasma electron beam welding system for earth orbiting vehicle)

Boring, K L ; Dickinson, T M ; Mc Murray, W ; Stauffer, L H ; Travis, E F

Plasma electron beam welder for space vehicles Final report (Feasibility of developing plasma electron beam welding system for earth orbiting vehicle), 1968, p.18P-18P

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4
Large-scale wind-tunnel investigation of an airplane model with a tilt wing of aspect ratio 8.4, and four propellers, in the presence of a ground plane (Aerodynamic characteristics of large-scale model of tilt-wing V/STOL aircraft)
Large-scale wind-tunnel investigation of an airplane model with a tilt wing of aspect ratio 8.4, and four propellers, in the presence of a ground plane (Aerodynamic characteristics of large-scale model of tilt-wing V/STOL aircraft)
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Large-scale wind-tunnel investigation of an airplane model with a tilt wing of aspect ratio 8.4, and four propellers, in the presence of a ground plane (Aerodynamic characteristics of large-scale model of tilt-wing V/STOL aircraft)

Deckert, W H ; Dickinson, S O ; Page, V R

Large-scale wind-tunnel investigation of an airplane model with a tilt wing of aspect ratio 8.4, and four propellers, in the presence of a ground plane (Aerodynamic characteristics of large-scale model of tilt-wing V/STOL aircraft), 1968, p.80P-80P

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5
Large-scale wind-tunnel tests of a deflected slipstream STOL model with wings of various aspect ratios (Wind tunnel determination of longitudinal force characteristics for STOL aircraft scale models with varying wing aspect ratios)
Large-scale wind-tunnel tests of a deflected slipstream STOL model with wings of various aspect ratios (Wind tunnel determination of longitudinal force characteristics for STOL aircraft scale models with varying wing aspect ratios)
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Large-scale wind-tunnel tests of a deflected slipstream STOL model with wings of various aspect ratios (Wind tunnel determination of longitudinal force characteristics for STOL aircraft scale models with varying wing aspect ratios)

Deckert, W H ; Dickinson, S O ; Page, V R

Large-scale wind-tunnel tests of a deflected slipstream STOL model with wings of various aspect ratios (Wind tunnel determination of longitudinal force characteristics for STOL aircraft scale models with varying wing aspect ratios), 1968, p.56P-56P

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6
Porosimetry data interpretation (Porosimetry data interpretation using statistical model for particle size analysis)
Porosimetry data interpretation (Porosimetry data interpretation using statistical model for particle size analysis)
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Porosimetry data interpretation (Porosimetry data interpretation using statistical model for particle size analysis)

Dickinson, J M ; Lewis, H D

Porosimetry data interpretation (Porosimetry data interpretation using statistical model for particle size analysis), 1968, p.13P-13P

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7
The use of stabilised steels in the PFR circuit (Use of stabilized steels in PFR circuits for protection from decarburization and loss of strength on exposure to sodium)
The use of stabilised steels in the PFR circuit (Use of stabilized steels in PFR circuits for protection from decarburization and loss of strength on exposure to sodium)
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The use of stabilised steels in the PFR circuit (Use of stabilized steels in PFR circuits for protection from decarburization and loss of strength on exposure to sodium)

Dickinson, F S ; Jackson, H ; Turner, F ; Watkins, B

The use of stabilised steels in the PFR circuit (Use of stabilized steels in PFR circuits for protection from decarburization and loss of strength on exposure to sodium), 1970, p.21P-21P

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8
The thermal degradation of perfluoropolypyridine (Thermal stability of perfluoro polypyridine and polytetrafluoroethylene thermal degradation products and fluorine weight analysis)
The thermal degradation of perfluoropolypyridine (Thermal stability of perfluoro polypyridine and polytetrafluoroethylene thermal degradation products and fluorine weight analysis)
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The thermal degradation of perfluoropolypyridine (Thermal stability of perfluoro polypyridine and polytetrafluoroethylene thermal degradation products and fluorine weight analysis)

Cotter, J L ; Dickinson, H ; Knight, G J ; Wright, W W

The thermal degradation of perfluoropolypyridine (Thermal stability of perfluoro polypyridine and polytetrafluoroethylene thermal degradation products and fluorine weight analysis), 1970, p.17P-17P

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9
The X-ray system of crystallographic programs for any computer having a PIDGIN FORTRAN compiler (X ray system for solving structure of crystals by diffraction techniques)
The X-ray system of crystallographic programs for any computer having a PIDGIN FORTRAN compiler (X ray system for solving structure of crystals by diffraction techniques)
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The X-ray system of crystallographic programs for any computer having a PIDGIN FORTRAN compiler (X ray system for solving structure of crystals by diffraction techniques)

Stewart, J M ; Kruger, G J ; Ammon, H L ; Dickinson, C ; Hall, S R

The X-ray system of crystallographic programs for any computer having a PIDGIN FORTRAN compiler (X ray system for solving structure of crystals by diffraction techniques), 1972, p.283P-283P

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10
Computation of possible climatic consequences of perturbations to stratospheric aerosols, ozone and water vapor with radiative-convective models [Final Report]
Computation of possible climatic consequences of perturbations to stratospheric aerosols, ozone and water vapor with radiative-convective models [Final Report]
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Computation of possible climatic consequences of perturbations to stratospheric aerosols, ozone and water vapor with radiative-convective models [Final Report]

COAKLEY, J A, J R ; Schneider, S H ; Dickinson, R E

Computation of possible climatic consequences of perturbations to stratospheric aerosols, ozone and water vapor with radiative-convective models [Final Report], 1975, p.24P-24P

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