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Robert L Stallings

9 cilt bulundu.

Cilt sonuçları

Laughing Space

Isaac Asimov, Janet Asimov, John Stallings, L. Sprague De Camp, Ogden Nash, Robert Hillyer, Russell Baker, Alan Edward Nourse, Alan Nelson, Jack C. Haldeman, Sherwood Springer, Katherine MacLean, Lion Miller, Gerald Jonas, Norman Kagan, D. F. Jones, Ludwig Bemelmans, Robert Grossbach, Theodore Sturgeon, George Gamow, Fred Hoyle, Ben Bova, A. J. Deutsch, Alfred Bester, Jesse F. Bone, Randall Garrett, Sansoucy Kathenor, Avram Davidson, Robert Sheckley, Jon Lucas, Fritz Leiber, Damon Knight, John M. Ford, Leo Szilard, Mary W. Stanton, Cam Thornley, Dian Girard, Larry T. Shaw, Arnie Bateman, Evelyn E. Smith, Frank Ramirez, Robert Arthur, Jack Finney, Anne Lear, Cynthia Goldstone, Al Sarrantonio, George Alec Effinger, Brad Cahoon, Thomas N. Scortia, Charles Beaumont, Chad Oliver, Raylyn Moore, K. J. Snow, Deborah Crawford, Kevin O'Donnell, Jr, Clifford D. Simak, Richard Matheson, Cyril M. Kornbluth, Patricia Nurse, Reginald Bretnor, Jon L. Breen, James T. Farrell, E. Y. Harburg, Bill Pronzini, Hal Draper · Robson Books Ltd

521 sayfa · 1982

American Science fiction / Pictorial American wit and humor / American wit and humor / Literature / American wit and humor, pictorial

WingsWing-alone aerodynamic characteristics for high angles of attack at supersonic speedsRobert L Stallings

Wing-alone aerodynamic characteristics for high angles of attack at supersonic speeds

Robert L Stallings · National Aeronautics and Space Administration, Scientific and Technical Information Branch

187 sayfa · 1981

Aerodynamics, Supersonic / Airplanes / Supersonic Aerodynamics / Wings

Supersonic wind tunnelsWind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3Robert L Stallings

Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3

Robert L Stallings · National Aeronautics and Space Administration, Scientific and Technical Information Branch

45 sayfa · 1980

Aerothermodynamics / Boundary layer / Supersonic wind tunnels

CiltMeasurements of store forces and moments and cavity pressures for a generic store in and near a box cavity at subsonic and transonic speedsRobert L. Stallings

Measurements of store forces and moments and cavity pressures for a generic store in and near a box cavity at subsonic and transonic speeds

Robert L. Stallings · National Aeronautics and Space Administration, Langley Research Center

Sayfa sayısı yok · 1995

Kategori yok

Stability of airplanesEffect of Reynolds number on stability characteristics of a cruciform wing-body at supersonic speedsRobert L Stallings

Effect of Reynolds number on stability characteristics of a cruciform wing-body at supersonic speeds

Robert L Stallings · for sale by the National Technical Information Service]

108 sayfa · 1980

Airplanes / Wings / Stability of airplanes

Aerodynamic loadMeasurements of forces, moments, and pressures on a generic store separating from a box cavity at supersonic speedsRobert L. Stallings

Measurements of forces, moments, and pressures on a generic store separating from a box cavity at supersonic speeds

Robert L. Stallings · For sale by the National Technical Information Service]

Sayfa sayısı yok · 1991

Cavities (Airplanes) / Aerodynamic load

Supersonic AerodynamicsExperimental cavity pressure distributions at supersonic speedsRobert L. Stallings

Experimental cavity pressure distributions at supersonic speeds

Robert L. Stallings · For sale by the National Technical Information Service]

Sayfa sayısı yok · 1987

Aerodynamics, Supersonic / Supersonic Aerodynamics

Supersonic AerodynamicsEffects of roughness size on the position of boundary-layer transition and on the aerodynamic characteristics of a 55ê swept delta wing at supersonic speedsRobert L Stallings

Effects of roughness size on the position of boundary-layer transition and on the aerodynamic characteristics of a 55ê swept delta wing at supersonic speeds

Robert L Stallings · for sale by the National Technical Information Service

47 sayfa · 1977

Aerodynamics, Supersonic / Boundary layer / Drag (Aerodynamics) / Supersonic Aerodynamics

Supersonic AerodynamicsAerodynamic characteristics of a Sparrow III missile model in the flow field of a generalized parent body at Mach 2.86Robert L Stallings

Aerodynamic characteristics of a Sparrow III missile model in the flow field of a generalized parent body at Mach 2.86

Robert L Stallings · For sale by the National Technical Information Service]

26 sayfa · 1984

Aerodynamics, Supersonic / Guided missiles / Supersonic Aerodynamics