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Authors

Author

John R. Spreiter

Books

Use of Source Distributions for Evaluating Theoretical Aerodynamics of Thin Finite Wings at Supersonic Speeds
Use of Source Distributions for Evaluating Theoretical Aerodynamics of Thin Finite Wings at Supersonic Speeds
United States. National Advisory Committee for Aeronautics, Harvard Lomax, John R. Spreiter, George J. Heimerl, Chung-Hua Wu, Arthur W. Goldstein, William M. Roberts, S. S. Manson, Max. A. Heaslet, John D. Stanitz, Dean R. Chapman, Artur Mager, Loma Sluder, A. J. Eggers, John C. Evvard, Gaylord O. Ellis, Lincoln Wolfestein
Impingement of Cloud Droplets on a Cylinder and Procedure for Measuring Liquid-water Content and Droplet Sizes in Supercooled Clouds by Rotating Multicylinder Method
Impingement of Cloud Droplets on a Cylinder and Procedure for Measuring Liquid-water Content and Droplet Sizes in Supercooled Clouds by Rotating Multicylinder Method
United States. National Advisory Committee for Aeronautics, Hermon M. Parker, Alfred Gessow, Norman S. Silsby, John R. Spreiter, Wilber B. Huston, T. H. Skopinski, E. R. G. Eckert, Kenneth B. Amer, Alberta Alksne, G. Chester Furlong, Georege J. Pack, A. J. Diagula, J. N. B. Livingood, Thomas V. Bollech, W. E. Phillips
Calculative Techniques for Transonic Flows about Certain Classes of Wing-body Combinations: Phase II
Calculative Techniques for Transonic Flows about Certain Classes of Wing-body Combinations: Phase II
John R. Spreiter, Stephen S. Stahara
Theoretical Prediction of Pressure Distributions on Nonlifting Airfoils at High Subsonic Speeds
Theoretical Prediction of Pressure Distributions on Nonlifting Airfoils at High Subsonic Speeds
John R. Spreiter, Alberta Alksne
A Study of the Simulation of Flow with Free-stream Mach Number 1 in a Choked Wind Tunnel
A Study of the Simulation of Flow with Free-stream Mach Number 1 in a Choked Wind Tunnel
John R. Spreiter, B. Jeanne Hyett, Donald W. Smith
Slender-body Theory Based on Approximate Solution of the Transonic Flow Equation
Slender-body Theory Based on Approximate Solution of the Transonic Flow Equation
John R. Spreiter, Alberta Y. Alksne
Torsional Stiffness of Thin-walled Shells Having Reinforcing Cores and Rectangular, Triangular, Or Diamond Cross Section
Torsional Stiffness of Thin-walled Shells Having Reinforcing Cores and Rectangular, Triangular, Or Diamond Cross Section
United States. National Advisory Committee for Aeronautics, Max A. Heaslet, John R. Spreiter, E. B. Klunker, Alberta Y. Alksne, George J. Nothwang, Harvey G. McComb, Henry H. Heyson, John H. Povolny, Keith C. Harder, Mitchel H. Bertram, Rinaldo J. Brun, W. E. Moeckel, Fred W. Steffen, S. Katzoff, Jack G. McArdle
Theoretical Determination of the Form of the Hollow Produced in the Solar Corpuscular Stream by Interaction with the Magnetic Dipole Field of the Earth
Theoretical Determination of the Form of the Hollow Produced in the Solar Corpuscular Stream by Interaction with the Magnetic Dipole Field of the Earth
John R. Spreiter, Benjamin R. Briggs
Theoretical Determination of the Form of the Hollow Produced in the Solar Corpuscular Stream by Interaction with the Magnetic Dipole Field of the Earth
Theoretical Determination of the Form of the Hollow Produced in the Solar Corpuscular Stream by Interaction with the Magnetic Dipole Field of the Earth
John R. Spreiter, Benjamin R. Briggs

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