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Harry W Carlson

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Jorge Luis Borges, Silvina Ocampo, Adolfo Bioy Casares, Ryūnosuke Akutagawa, Thomas Bailey Aldrich, Леонид Николаевич Андреев, John Aubrey, J. G. Ballard, Sir Max Beerbohm, Ambrose Bierce, Ah'med Ech Chiruani, Léon Bloy, Delia Ingenieros, Ray Bradbury, Tor Åge Bringsværd, Martin Buber, Richard Francis Burton, Arturo Cancela, Pilar de Lusarreta, Thomas Carlyle, Lewis Carroll, Gilbert Keith Chesterton, Zhuangzi, Jean Cocteau, Julio Cortázar, Santiago Dabove, Alexandra David-Néel, Lord Edward Dunsay, Macedonio Fernandez, James George Frazer, Elena Garro, Herbert Allen Giles, Nathaniel Hawthorne, I. A. Ireland, W. W. Jacobs, James Joyce, Don Juan Manuel, Franz Kafka, Rudyard Kipling, Leopoldo Lugones, Arthur Machen, Walter De la Mare, Guy de Maupassant, Edwin Morgan, H. A. Murena, Niu Chiao, Papini, Giovanni, Carlos Peralta, Barry Perowne, Petronius, Manuel Peyrou, Edgar Allan Poe, Pu Songling, François Rabelais, Saki, May Sinclair, Walter W. Skeat, Olaf Stapledon, Emanuel Swedenborg, Лев Толстой, B. Traven, Tsʻao, Hsüeh-chʻin., Auguste comte de Villiers de L'Isle-Adam, Voltaire, Evelyn Waugh, Edward Lucas White, Juan Rodolfo Wilcock, Oscar Wilde, Richard Wilhelm, G. Willoughby-Meade, Mary Shelley, Wu Cheng'en, William Butler Yeats, Jose Zorilla · Xanadu

407 sayfa · 1940

Fantasy literature / Fantastic literature / Anachronisms / speculative fiction / subjective idealism

The United States in Literature [with three long stories] -- Seventh Edition

Isaac Asimov Presents Tales of the Occult

Isaac Asimov, Martin H. Greenberg, Charles G. Waugh, H. G. Wells, Rudyard Kipling, Henry Slesar, Gertrude Henderson, Nathaniel Hawthorne, Helen McCloy, Kris Neville, Edgar Allan Poe, Edward Bulwer Lytton, Baron Lytton, Manly Wade Wellman, · Plaza y Janes

Leading edges (Aerodynamics)Estimation of leading-edge thrust for supersonic wings of arbitrary planformHarry W Carlson

Estimation of leading-edge thrust for supersonic wings of arbitrary planform

Harry W Carlson · for sale by the National Technical Information Service.

46 sayfa · 1978

Supersonic planes / Airplanes / Wings / Leading edges (Aerodynamics)

Shock wavesSimplifed sonic-boom predictionHarry W Carlson

Simplifed sonic-boom prediction

Harry W Carlson · for sale by the National Technical Information Service

48 sayfa · 1978

Sonic boom / Shock waves

Reusable space vehiclesA wind-tunnel study of the applicability of far-field sonic-boom theory to the space shuttle orbiterHarry W Carlson

A wind-tunnel study of the applicability of far-field sonic-boom theory to the space shuttle orbiter

Harry W Carlson · National Aeronautics and Space Administration, Scientific and Technical Information Office

45 sayfa · 1978

Wind tunnels / Sonic boom / Reusable space vehicles

WingsEstimation of attainable leading-edge thrust for wings at subsonic and supersonic speedsHarry W Carlson

Estimation of attainable leading-edge thrust for wings at subsonic and supersonic speeds

Harry W Carlson · National Aeronautics and Space Administration, Scientific and Technical Information Branch

59 sayfa · 1979

Testing / Airplanes / Thrust / Motors / Wings

Flaps (Airplanes)Validation of a computer code for analysis of subsonic aerodynamic performance of wings with flaps in combination with a canard or horizontal tail and an application of optimizationHarry W. Carlson

Validation of a computer code for analysis of subsonic aerodynamic performance of wings with flaps in combination with a canard or horizontal tail and an application of optimization

Harry W. Carlson · National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division

Sayfa sayısı yok · 1990

Aerodynamics / Airplanes / Canard Wings / Computer simulation / Flaps (Airplanes)

TestingA study of the sonic-boom characteristics of a blunt body at a Mach number of 4.14Harry W. Carlson

A study of the sonic-boom characteristics of a blunt body at a Mach number of 4.14

Harry W. Carlson · for sale by the National Technical Information Service

28 sayfa · 1977

Aerodynamics, Supersonic / Sonic boom / Space vehicles / Supersonic Aerodynamics / Testing

Numerical analysisApplicability of linearized-theory attached-flow methods to design and analysis of flap systems at low speeds for thin swept wings with sharp leading edgesHarry W. Carlson

Applicability of linearized-theory attached-flow methods to design and analysis of flap systems at low speeds for thin swept wings with sharp leading edges

Harry W. Carlson · For sale by the National Technical Information Service]

Sayfa sayısı yok · 1987

Aerodynamics / Numerical analysis

WingsSurvey and analysis of research on supersonic drag-due-to-lift minimumization with recommendations for wing designHarry W. Carlson

Survey and analysis of research on supersonic drag-due-to-lift minimumization with recommendations for wing design

Harry W. Carlson · National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program

Sayfa sayısı yok · 1992

Aerodynamics, Supersonic / Airplanes / Supersonic Aerodynamics / Wings

Canard configurationsValidation of a computer code for analysis of subsonic aerodynamic performance of wings with flaps in combination with a canard or horizontal tail and an application to optimizationHarry W. Carlson

Validation of a computer code for analysis of subsonic aerodynamic performance of wings with flaps in combination with a canard or horizontal tail and an application to optimization

Harry W. Carlson · Langley Research center

122 sayfa · 1990

Flaps / Canard configurations

Leading edge thrustImproved method for prediction of attainable wing leading-edge thrustHarry W. Carlson

Improved method for prediction of attainable wing leading-edge thrust

Harry W. Carlson · Langley Research Center

60 sayfa · 1996

Leading edge thrust

CiltSimplified sonic-boom predictionHarry W. Carlson

Simplified sonic-boom prediction

Harry W. Carlson · National Aeronautics and Space Administration Scientific and Technical Information Office

Sayfa sayısı yok · 1978

Kategori yok

AirplanesValidation of a pair of computer codes for estimation and optimization of subsonic aerodynamic performance of simple hinged-flap systems for thin swept wingsHarry W. Carlson

Validation of a pair of computer codes for estimation and optimization of subsonic aerodynamic performance of simple hinged-flap systems for thin swept wings

Harry W. Carlson · National Aeronautics and Space Administration, Scientific and Technical Information Division

Sayfa sayısı yok · 1988

Wings, Swept-back / Aerodynamics / Airplanes

WingsSurvey and analysis of research on supersonic drag-due-to-lift minimization with recommendations for wing designHarry W. Carlson

Survey and analysis of research on supersonic drag-due-to-lift minimization with recommendations for wing design

Harry W. Carlson · Langley Research Center

153 sayfa · 1992

Lift / Supersonic drag / Wings

WingsEstimation of wing nonlinear aerodynamic characteristics at supersonic speedsHarry W Carlson

Estimation of wing nonlinear aerodynamic characteristics at supersonic speeds

Harry W Carlson · For sale by the National Technical Information Service]

81 sayfa · 1980

Aerodynamics, Supersonic / Airplanes / Supersonic Aerodynamics / Supersonic planes / Wings

System analysisA modificiation to linearized theory for prediction of pressure loadings on lifting surfaces at high supersonic Mach numbers and large angles of attackHarry W Carlson

A modificiation to linearized theory for prediction of pressure loadings on lifting surfaces at high supersonic Mach numbers and large angles of attack

Harry W Carlson · for sale by the National Technical Information Service

36 sayfa · 1979

Aerodynamic load / Aerodynamics, Supersonic / Supersonic Aerodynamics / System analysis

WingsThe design and analysis of simple low speed flap systems with the aid of linearized theory computer programsHarry W. Carlson

The design and analysis of simple low speed flap systems with the aid of linearized theory computer programs

Harry W. Carlson · National Aeronautics and Space Administration, Scientific and Technical Information Branch

Sayfa sayısı yok · 1987

Computer programs / Aerodynamics / Airplanes / Wings

CiltNumerical methods and a computer program for subsonic and supersonic aerodynamic design and analysis of wings with attainable thrust considerationsHarry W Carlson

Numerical methods and a computer program for subsonic and supersonic aerodynamic design and analysis of wings with attainable thrust considerations

Harry W Carlson · National Technical Information Service, distributor]

Sayfa sayısı yok · 1984

Kategori yok

System analysisA modification to linearized theory for prediction of pressure loadings on lifting surfaces at high supersonic Mach numbers and large angles of attackHarry W. Carlson

A modification to linearized theory for prediction of pressure loadings on lifting surfaces at high supersonic Mach numbers and large angles of attack

Harry W. Carlson · National Aeronautics and Space Administration, Scientific and Technical Information Office

36 sayfa · 1979

Aerodynamic load / Aerodynamics, Supersonic / Supersonic Aerodynamics / System analysis

WingsApplication of an aerodynamic analysis method including attainable thrust estimates to low speed leading-edge flap design for supersonic cruise vehiclesHarry W. Carlson

Application of an aerodynamic analysis method including attainable thrust estimates to low speed leading-edge flap design for supersonic cruise vehicles

Harry W. Carlson · National Aeronautics and Space Administration, Langley Research Center

Sayfa sayısı yok · 1985

Aerodynamics / Airplanes / Wings

Mathematical modelsA computer program for wing subsonic aerodynamic performance estimates including attainable thrust and vortex lift effectsHarry W Carlson

A computer program for wing subsonic aerodynamic performance estimates including attainable thrust and vortex lift effects

Harry W Carlson · For sale by the National Technical Information Service]

59 sayfa · 1982

Aerodynamics / Data processing / Mathematical models