Search Results - Landrum, Emma Jean
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1
Wind-tunnel force and flow visualization data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4̊ to 60̊ / by Landrum, Emma Jean
Published 1979Call Number: Loading…Search for the full-text version of this title in HathiTrust
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2
Wind-tunnel pressure data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4̊ to 60̊ / by Landrum, Emma Jean
Published 1977Call Number: Loading…Search for the full-text version of this title in HathiTrust
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3
Effect of shape changes on the aerodynamic characteristics of a twisted and cambered arrow wing at Mach number 2.03 / by Landrum, Emma Jean, Shrout, Barrett L.
Published 1968Call Number: Loading…Online Access
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4
Compilation of information on the transonic attachment of flows at the leading edges of airfoils / by Lindsey, W. F.
Published 1958Other Authors: “…Landrum, Emma Jean…”
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5
Theoretical and experimental study of twisted and cambered delta wings designed for a Mach number of 3.5 / by Sorrells, Russell B.
Published 1976Other Authors: “…Landrum, Emma Jean…”
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Related Subjects
Body of revolution
Flow visualization
Wind tunnels
Aerodynamic load
Aerodynamics
Aerodynamics, Supersonic
Aerodynamics, Transonic
Aerofoils
Airplanes
Camber (Aerofoils)
Control systems
Guided missiles
Leading edges (Aerodynamics)
Mach number
Measurement
Pressure
Reynolds number
Schlieren photography
Strain gages
Wings