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Primary view of Comparison of the performance of a helicopter-type ram-jet engine under various centrifugal loadings
Radin, Edward J. & Carpenter, Paul J.
October 7, 1953
Primary view of Rocket-Model Investigation to Determine the Hinge-Moment and Normal-Force Properties of a Full-Span, Constant-Chord, Partially Balanced Trailing-Edge Control on a 60 Degree Clipped Delta Wing Between Mach Numbers of 0.50 and 1.26
Martz, C. William & Goslee, John W.
October 30, 1953
Primary view of A pressure-distribution investigation of a fineness-ratio-12.2 parabolic body of revolution (NACA RM-10) at M = 1.59 and angles of attack up to 36 degrees
Cooper, Morton; Gapcynski, John P. & Hasel, Lowell E.
October 30, 1952
Primary view of Heat-Exchanger-Core Weights for Use With Hydrogen-Expansion Turbine
Reynolds, Thaine W.
October 3, 1957
Primary view of Simulator studies of a simple homing system
Passera, Anthony L. & Garner, H. Douglas
October 6, 1955
Primary view of An Experimental Investigation of the Flow Phenomena Over Bodies at High Angles of Attack at a Mach Number of 2.01
Gapcynski, John P.
October 27, 1955
Primary view of Statistical measurements of landing contact conditions of the Boeing B-47 airplane
Kolnick, Joseph J. & Morris, Garland J.
October 27, 1955
Primary view of Modified tubular combustor as high-temperature gas generators
Friedman, Robert & Zettle, Eugene V.
October 21, 1955
Primary view of Drag and rolling-moment effectiveness of trailing-edge spoilers at Mach numbers 2.2 and 5.0
Canning, Thomas N. & DeRose, Charles E.
October 3, 1955
Primary view of Free-flight investigation to obtain drag-at-lift and stability data for a 60 degree delta-wing-body configuration over a Mach number range of 1.3 to 1.6
Welsh, Clement J.
October 6, 1955
Primary view of Flight measurements of directional stability to a Mach number of 1.48 for an airplane tested with three different vertical tail configurations
Drake, Hubert M.; Finch, Thomas W. & Peele, James R.
October 7, 1955
Primary view of Wind-Tunnel Investigation of the Static Longitudinal and Lateral Stability of the Bell X-1A at Supersonic Speeds
Henderson, Arthur, Jr.
October 27, 1955
Primary view of Temperature Recovery Factors on a Slender 12 Degree Cone-Cylinder at Mach Numbers From 3.0 to 6.3 and Angles of Attack Up to 45 Degrees
Reller, John O. & Hamaker, Frank M.
October 3, 1955
Primary view of Investigation of a Three-Stage Transonic Research Axial-Flow Compressor: Aerodynamic Design and Overall Performance
Savage, Melvyn & Beatty, Loren A.
October 27, 1955
Primary view of A theoretical analysis of the effect of engine angular momentum on longitudinal and directional stability in steady rolling maneuvers
Gates, Ordway B., Jr. & Woodling, C. H.
October 7, 1955
Primary view of Calculated Heats of Formation and Combustion of Boron Compounds (Boron, Hydrogen, Carbon, Silicon)
Altshuller, Aubrey P.
October 4, 1955
Primary view of A Theoretical Analysis of a Simple Aerodynamic Device to Improve the Longitudinal Damping of a Cruciform Missile Configuration at Supersonic Speeds
Clements, James E.
October 27, 1955
Primary view of Flight measurements of the vertical-tail loads on the Convair XF-92A delta-wing airplane
Johnson, Clinton T.
October 27, 1955
Primary view of The Effect of Wing Profile on the Transonic Characteristics of Rectangular and Triangular Wings Having Aspect Ratios of 3: Transonic Bump Technique
Nelson, Warren H. & Frank, Joseph L.
October 27, 1954
Primary view of Effects of angle of attack and airfoil profile on the two-dimensional flutter derivatives for airfoils oscillating in pitch at high subsonic speeds
Wyss, John A. & Herrera, Raymond
October 15, 1954
Primary view of Effects of Secondary-Air Flow on Annular Base Force of a Supersonic Airplane
Vargo, Donald J.
October 11, 1954
Primary view of Investigation of the NACA 4-(5)(05)-037 six- and eight-blade, dual-rotation propellers at positive and negative thrust at Mach numbers up to 0.90, including some aerodynamic characteristics of the NACA 4-(5)(05)-041 two- and four-blade, single-rotat
Walker, John H. & Reynolds, Robert M.
October 8, 1954
Primary view of Analytical Study of the Effect of Center-of-Gravity Position on the Response to Longitudinal Control in Landing Approaches of a Swept-Wing Airplane of Low Aspect Ratio Having No Horizontal Tail
Stone, Ralph W., Jr.
October 15, 1954
Primary view of Wind pressure distributions at low lift for the XF-92A delta-wing airplane at transonic speeds
Keener, Earl R.
October 20, 1954
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