Search Results

Primary view of Analysis of a Nuclear-Powered Liquid-Metal Ducted-Fan Cycle
Rom, F. E. & Wachtl, W. W.
December 17, 1952
Primary view of Arrangement of Bodies of Revolution in Supersonic Flow to Reduce Wave Drag
Friedman, Morris D.
December 17, 1951
Primary view of Design and Evaluation of a Turbojet Exhaust Simulator, Utilizing a Solid-Propellant Rocket Motor, for Use in Free-Flight Aerodynamic Research Models
de Moraes, Carlos A.; Hagginbothom, William K., Jr. & Falanga, Ralph A.
December 17, 1954
Primary view of Investigation at Supersonic Speeds of the Effect of Jet Mach Number and Divergence Angle of the Nozzle Upon the Pressure of the Base Annulus of a Body of Revolution
Bromm, August F., Jr. & O'Donnell, Robert M.
December 17, 1954
Primary view of The effect of stick-force gradient and stick gearing on the tracking accuracy of a fighter airplane
Abramovitz, Marvin & Van Dyke, Rudolph D., Jr.
December 17, 1954
Primary view of Wind-tunnel investigation of horizontal tails 3: unswept and 35 degrees swept-back plan forms of aspect ratio 6
Dods, Jules B., Jr.
December 17, 1948
Primary view of Analysis of a Nuclear-Powered Liquid-Metal Ducted-Fan Cycle
Rom, F. E. & Wachtl, W. W.
December 17, 1952
Primary view of Full-scale investigation of cooling shroud and ejector nozzle for a turbojet engine: afterburner installation
Wallner, Lewis E. & Jansen, Emmert T.
December 17, 1951
Primary view of An Investigation of the Aerodynamic Characteristics of a Series of Cone-Cylinder Configurations at a Mach Number of 6.86
Cooper, Ralph D. & Robinson, Raymond A.
December 17, 1951
Primary view of Comparison of drag, pressure recovery, and surface pressure of a scoop-type inlet and an NACA submerged inlet at transonic speeds
Frank, Joseph L. & Taylor, Robert A.
December 17, 1951
Primary view of Effects of rigid spoilers on the two-dimensional flutter derivatives of airfoils oscillating in pitch at high subsonic speeds
Monfort, James C. & Wyss, John A.
December 17, 1954
Primary view of Lateral Motions Encountered with the Douglas D-558-II All-Rocket Research Airplane During Exploratory Flights to a Mach Number of 2.0
Ankenbruck, Herman O. & Wolowicz, Chester H.
December 17, 1954
Primary view of Preliminary Investigation of Use of Conical Flow Separation for Efficient Supersonic Diffusion
Moeckel, W. E. & Evans, P. J., Jr.
December 17, 1951
Primary view of Arrangement of Bodies of Revolution in Supersonic Flow to Reduce Wave Drag
Friedman, Morris D.
December 17, 1951
Back to Top of Screen