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Primary view of Additional results of an investigation at transonic speeds to determine the effects of a heated propulsive jet on the drag characteristics of a series of related afterbodies
Henry, Beverly Z., Jr. & Cahn, Maurice S.
September 24, 1956
Primary view of Aerodynamic Characteristics of a 45 Degree Swept Wing Fighter Airplane Model and Aerodynamic Loads on Adjacent Stores and Missiles at Mach Numbers of 1.57, 1.87, 2.16, and 2.53
Oehman, Waldo I. & Turner, Kenneth L.
June 24, 1958
Primary view of Aerodynamic Characteristics of a 45 Degree Swept-Wing Fighter-Airplane Model and Aerodynamic Loads on Adjacent Stores and Missiles at Mach Numbers of 1.57, 1.87, 2.16, and 2.53
Oehman, Waldo I. & Turner, Kenneth L.
June 24, 1958
Primary view of Aerodynamic characteristics of a canard and an outboard-tail airplane model at a Mach number of 2.01
Spearman, M. Leroy & Robinson, Ross B.
March 24, 1958
Primary view of Aerodynamic characteristics of a wing with quarter-chord line swept back 60 degrees, aspect ratio 2, taper ratio 0.6, and NACA 65A006 airfoil section : transonic bump method
Myers, Boyd C., II & King, Thomas J., Jr.
February 24, 1950
Primary view of Aerodynamic characteristics of several jet-spoiler controls on a 45 degree sweptback wing at Mach numbers of 1.61 and 2.01
Lord, Douglas R.
June 24, 1958
Primary view of The Aerodynamic Characteristics of Two Series of Lifting Bodies at Mach Number 6.86
Ridyard, Herbert W.
May 24, 1954
Primary view of Aerodynamic Loads on an External Store Adjacent to a 60 Degree Delta Wing at Mach Numbers From 0.75 to 1.96
Hadaway, William M.
April 24, 1956
Primary view of An analog study of the relative importance of various factors affecting roll coupling
Weil, Joseph & Day, Richard E.
April 24, 1956
Primary view of Analysis of Fluorine Addition to the Vanguard First Stage
Tomazic, William A.; Schmidt, Harold W. & Tischler, Adelbert O.
January 24, 1957
Primary view of Analysis of fluorine addition to the vanguard first stage
Tomazic, William A.; Schmidt, Harold W. & Tischler, Adelbert O.
January 24, 1957
Primary view of Application of supersonic vortex-flow theory to the design of supersonic impulse compressor- or turbine-blade sections
Boxer, Emanuel; Sterrett, James R. & Wlodarski, John
April 24, 1952
Primary view of Axial-Slot Air Admission for Controlling Performance of a One-Quarter-Annual Turbojet Combustor and Comparison With Complete Engine
Mark, Herman & Zettle, Eugene V.
March 24, 1952
Primary view of Behavior of Some Materials and Shapes in Supersonic Free Jets at Stagnation Temperatures Up to 4,210 Degrees F, and Descriptions of the Jets
Fields, E. M.; Hopko, Russell N.; Swain, Robert L. & Trout, Otto F., Jr.
February 24, 1958
Primary view of Blow-Out Velocities of Solutions of Hydrocarbons and Boron Hydride - Hydrocarbon Reaction Products in a 1 7/8-Inch-Diameter Combustor
Morris, James F. & Lord, Albert M.
October 24, 1957
Primary view of A Brief Investigation of the Effect of Waves on the Take-Off Resistance of a Seaplane
Mottard, Elmo J.
April 24, 1956
Primary view of Buffeting of a vertical tail on an inclined body at supersonic Mach numbers
Gowen, Forrest E.
March 24, 1953
Primary view of Calculation of the Lateral Stability of a Directly Coupled Tandem-Towed Fighter Airplane and Correlation with Experimental Data
Shanks, Robert E.
June 24, 1958
Primary view of Calculations of Laminar Heat Transfer Around Cylinders of Arbitrary Cross Section and Transpiration-Cooled Walls with Application to Turbine Blade Cooling
Eckert, E. R. G. & Livingood, John N. B.
September 24, 1951
Primary view of Chordwise pressure distribution at high subsonic speeds near midsemispan of a tapered 35 degree sweptback wing of aspect ratio 4 having NACA 65A006 airfoil sections and equipped with various spoiler ailerons
Hammond, Alexander D. & McMullan, Barbara M.
June 24, 1952
Primary view of A comparative analysis of the performance of long-range hypervelocity vehicles
Eggers, Alfred J., Jr.; Allen, H. Julian & Neice, Stanford E.
March 24, 1955
Primary view of Comparison of effect of a turbojet engine and three cold-flow configurations on the stability of a full-scale supersonicle inlet
Musial, Norman T.
January 24, 1957
Primary view of Comparison of effects of ailerons and combinations of spoiler-slot-deflector arrangements on spin recovery of sweptback-wing model having mass distributed along the fuselage
Healy, Frederick M. & Klinar, Walter J.
November 24, 1954
Primary view of Comparison of the Minimum Drag of Two Versions of a Modified Delta-Wing Fighter as Obtained From Flight Tests of Rocket-Boosted Models and Equivalent Bodies Between Mach Numbers of 0.80 and 1.64
Hastings, Earl C., Jr. & Mitcham, Grady L.
September 24, 1956
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