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1
Three-dimensional transonic flow theory applied to slender wings and bodies / by Heaslet, M. A. (Maxwell Alfred), 1907-
Published 1956Call Number: Loading…
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2
Particular solutions for flows at Mach number 1 / by Heaslet, M. A. (Maxwell Alfred), 1907-
Published 1956Call Number: Loading…
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3
The calculation of pressure on slender airplanes in subsonic and supersonic flow / by Heaslet, M. A. (Maxwell Alfred), 1907-
Published 1953Call Number: Loading…
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4
The minimization of wave drag for wings and bodies with a given base area or volume / by Heaslet, M. A. (Maxwell Alfred), 1907-
Published 1954Call Number: Loading…
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5
Drag minimization for wings in supersonic flow, with various constraints / by Heaslet, M. A. (Maxwell Alfred), 1907-
Published 1958Call Number: Loading…
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6
Reciprocity relations in aerodynamics / by Heaslet, M. A. (Maxwell Alfred), 1907-
Published 1952Call Number: Loading…Search for the full-text version of this title in HathiTrust
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7
Axially symmetric shapes with minimum wave drag / by Heaslet, M. A. (Maxwell Alfred), 1907-
Published 1955Call Number: Loading…
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8
Compressible potential flow with circulation about a circular cylinder / by Heaslet, M. A. (Maxwell Alfred), 1907-
Published 1944Call Number: Loading…
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9
Numerical predictions of radiative interchange between conducting fins with mutual irradiations / by Heaslet, M. A. (Maxwell Alfred), 1907-
Published 1961Call Number: Loading…
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10
Critical Mach numbers of thin airfoil sections with plain flaps / by Heaslet, M. A. (Maxwell Alfred), 1907-
Published 1946Call Number: Loading…
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11
Theoretical investigation of methods for computing drag from wake surveys at high subsonic speeds / by Heaslet, M. A. (Maxwell Alfred), 1907-
Published 1945Call Number: Loading…
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12
The Use of source-sink and doublet distributions extended to the solution of arbitrary boundary value problems in supersonic flow / by Heaslet, M. A. (Maxwell Alfred), 1907-
Published 1948Call Number: Loading…
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13
Volterra's solution of the wave equation as applied to three-dimensional supersonic airfoil problems / by Heaslet, M. A. (Maxwell Alfred), 1907-
Published 1947Call Number: Loading…Search for the full-text version of this title in HathiTrust
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14
The Calculation of downwash behind supersonic wings with an application to triangular plan forms / by Heaslet, M. A. (Maxwell Alfred), 1907-
Published 1948Call Number: Loading…Search for the full-text version of this title in HathiTrust
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15
Linearized compressible-flow theory for sonic flight speeds / by Heaslet, M. A. (Maxwell Alfred), 1907-
Published 1949Call Number: Loading…
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16
Two-dimensional unstead lift problems in supersonic flight / by Heaslet, M. A. (Maxwell Alfred), 1907-
Published 1948Call Number: Loading…
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17
The Application of Green's theorem to the solution of boundary-value problems in linearized supersonic wing theory / by Heaslet, M. A. (Maxwell Alfred), 1907-
Published 1949Call Number: Loading…
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18
Elementary number theory / by Uspensky, J. V. (James Victor), 1883-1947, Heaslet, M. A. (Maxwell Alfred), 1907-
Published 1939Call Number: Loading…
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19
Generalized conical-flow fields in supersonic wing theory / by Lomax, Harvard
Published 1951Other Authors: “…Heaslet, M. A. (Maxwell Alfred), 1907-…”
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20
Damping-in-roll calculations for slender swept-back wings and slender wing-body combinations / by Lomax, Harvard
Published 1949Other Authors: “…Heaslet, M. A. (Maxwell Alfred), 1907-…”
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Related Subjects
Airplanes
Aerodynamics, Supersonic
Mathematical analysis
Mathematics
Aerodynamics
Aerofoils
Wings
Drag (Aerodynamics)
Lift (Aerodynamics)
Air flow
Boundary value problems
Unsteady flow (Aerodynamics)
Aerodynamic load
Aerodynamics, Transonic
Aeronautics
Aircraft engines
Aircraft parts
Body of revolution
Charts, diagrams, etc
Cylinders
Differential equations, Partial
Fluid dynamics
Numerical solutions
Pitching (Aerodynamics)
Transportation research
Wings, Triangular
Aspect ratio (Aerofoils)
Compressibility
Cone
Downwash (Aerodynamics)