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1
Generalized conical-flow fields in supersonic wing theory / by Lomax, Harvard
Published 1951Call Number: Loading…
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2
Three-dimensional unsteady lift problems in high-speed flight : the triangular wing / by Lomax, Harvard
Published 1951Call Number: Loading…Search for the full-text version of this title in HathiTrust
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3
The indicial lift and pitching moment for a sinking or pitching two-dimensional wing flying at subsonic or supersonic speeds / by Lomax, Harvard
Published 1951Call Number: Loading…
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4
Three-dimensional, unsteady-lift problems in high-speed flight : basic concepts / by Lomax, Harvard
Published 1950Call Number: Loading…Search for the full-text version of this title in HathiTrust
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5
Formulas for source, doublet, and vortex distributions in supersonic wing theory / by Lomax, Harvard
Published 1950Call Number: Loading…
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6
Chordwise and compressibility corrections to slender-wing theory / by Lomax, Harvard
Published 1951Call Number: Loading…Search for the full-text version of this title in HathiTrust
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7
Theoretical aerodynamic characteristics of a family of slender wing-tail-body combinations / by Lomax, Harvard
Published 1951Call Number: Loading…
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8
Wing-body combinations with certain geometric restraints having low zero-lift wave drag at low supersonic Mach numbers / by Lomax, Harvard
Published 1956Call Number: Loading…
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9
Generalized indicial forces on deforming rectangular wings in supersonic flight / by Lomax, Harvard
Published 1954Call Number: Loading…
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10
A method for the calculation of wave drag on supersonic-edged wings and biplanes / by Lomax, Harvard
Published 1958Call Number: Loading…
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11
Lift developed on unrestrained rectangular wings entering gusts at subsonic and supersonic speeds / by Lomax, Harvard
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12
Stable implicit and explicit numerical methods for integrating quasi-linear differential equations with parasitic-stiff and parasitic-saddle eigenvalues / by Lomax, Harvard
Published 1968Call Number: Loading…Online Access
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13
Damping-in-roll calculations for slender swept-back wings and slender wing-body combinations / by Lomax, Harvard
Published 1949Call Number: Loading…Search for the full-text version of this title in HathiTrust
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14
Linearized lifting-surface theory for swept-back wings with slender plan forms / by Lomax, Harvard
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15
Two-dimensional, supersonic, linearized flow with heat addition / by Lomax, Harvard
Published 1959Call Number: Loading…
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16
An operational unification of finite difference methods for the numerical integration of ordinary differential equations / by Lomax, Harvard
Published 1967Call Number: Loading…
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17
Numerical analysis of flow properties about blunt bodies moving at supersonic speeds in an equilibrium gas / by Lomax, Harvard
Published 1964Call Number: Loading…
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18
Eigensystem analysis of classical relaxation techniques with applications to multigrid analysis by Lomax, Harvard
Published 1987Call Number: Loading…
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19
Downwash in the vertical and horizontal planes of symmetry behind a triangular wing in supersonic flow / by Lomax, Harvard
Published 1949Call Number: Loading…
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20
Sideslip angles and vertical-tail loads developed by periodic control deflections / by Lomax, Harvard
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Related Subjects
Airplanes
Aerodynamics, Supersonic
Wings
Mathematical analysis
Lift (Aerodynamics)
Numerical solutions
Aerodynamics
Aerofoils
Aerodynamic load
Air flow
Boundary value problems
Differential equations, Partial
Drag (Aerodynamics)
Mathematics
Unsteady flow (Aerodynamics)
Wings, Triangular
Aerodynamics, Transonic
Aeronautics
Aircraft engines
Aircraft parts
Control
Differential equations
Downwash (Aerodynamics)
Fuselage
Integral equations
Mathematical models
Numerical analysis
Pitching (Aerodynamics)
Rolling (Aerodynamics)
Tail surfaces