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1
An analysis of base pressure at supersonic velocities and comparison with experiment / by Chapman, Dean R.
Published 1950Call Number: Loading…
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2
Experimental investigation of base pressure on blunt-trailing-edge wings at supersonic velocities / by Chapman, Dean R.
Published 1952Call Number: Loading…Search for the full-text version of this title in HathiTrust
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3
Airfoil profiles for minimum pressure drag at supersonic velocities - general analysis with application to linearized supersonic flow / by Chapman, Dean R.
Published 1951Call Number: Loading…
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4
Reduction of profile drag at supersonic velocities by the use of airfoil sections having a blunt trailing edge / by Chapman, Dean R.
Published 1955Call Number: Loading…
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5
Effect of trailing-edge thickness on lift at supersonic velocities / by Chapman, Dean R.
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6
A theoretical analysis of heat transfer in regions of separated flow / by Chapman, Dean R.
Published 1956Call Number: Loading…
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7
Airfoil profiles for minimum pressure drag at supersonic velocities - application of shock-expansion theory, including consideration of hypersonic range / by Chapman, Dean R.
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8
Some possibilities of using gas mixtures other than air in aerodynamic research / by Chapman, Dean R.
Published 1954Call Number: Loading…Search for the full-text version of this title in HathiTrust
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9
Turbulent boundary-layer and skin-friction measurements in axial flow along cylinders at Mach numbers between 0.5 and 3.6 / by Chapman, Dean R.
Published 1954Call Number: Loading…
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10
Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition / by Chapman, Dean R.
Published 1957Call Number: Loading…
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11
An approximate analytical method for studying entry into planetary atmospheres / by Chapman, Dean R.
Published 1958Call Number: Loading…
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12
Airfoil profiles for minimum pressure drag at supersonic velocities - application of shock-expansion theory, including consideration of hypersonic range / by Chapman, Dean R.
Published 1952Call Number: Loading…Online Access
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13
An analysis of base pressure at supersonic velocities and comparison with experiment / by Chapman, Dean R.
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14
Investigation of slipstream effects on a wing-inlet oil-cooler ducting system of a twin-engine airplane in the Ames 40- by 80-foot wing tunnel / by Chapman, Dean R.
Published 1945Call Number: Loading…
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15
An analysis of the corridor and guidance requirements for supercircular entry into planetary atmospheres / by Chapman, Dean R.
Published 1960Call Number: Loading…
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16
Tables of z functions for atmosphere entry analyses / by Chapman, Dean R.
Published 1961Call Number: Loading…
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17
An approximate analytical method for studying entry into planetary atmospheres / by Chapman, Dean R.
Published 1959Call Number: Loading…(paper)
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18
Aerodynamic evidence pertaining to the entry of tektites into the earth's atmosphere / by Chapman, Dean R.
Published 1962Call Number: Loading…
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19
Laminar mixing of a compressible fluid / by Chapman, Dean R.
Published 1949Call Number: Loading…
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20
Turbulent skin friction at high Mach numbers and Reynolds numbers in air and helium / by Matting, Fred W.
Published 1961Other Authors: “…Chapman, Dean R.…”
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Related Subjects
Aerodynamics, Supersonic
Aerofoils
Air flow
Airplanes
Atmospheric entry
Drag (Aerodynamics)
Aerodynamic load
Aerodynamics
Aeronautics
Axial flow
Boundary layer
Mach number
Space vehicles
Trailing edges (Aerodynamics)
Aircraft engines
Aircraft parts
Inviscid flow
Reynolds number
Skin friction (Aerodynamics)
Transportation research
Wind tunnels
Ablation (Aerothermodynamics)
Air ducts
Artificial satellites
Atmospheric braking
Control systems
Cylinders
Differential equations
Fluid dynamics
Gases