Technical Report Archive & Image Library (TRAIL) - 991 Matching Results

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Primary view of 4-Channel Line Driver: Modified
Titterton, E. W.
1950?
Primary view of An 8-Foot Axisymmetrical Fixed Nozzle for Subsonic Mach Numbers Up to 0.99 and for a Supersonic Mach Number of 1.2
Ritchie, Virgil S.; Wright, Ray H. & Tulin, Marshall P.
February 23, 1950
Primary view of "25" Critically Consultation with J. W. Morfitt : April 3, 1950
Merrill, E. T. & Sege, G.
April 3, 1950
Primary view of 30 Rv. Power Supply
U.S. Atomic Energy Commission
1950?
Primary view of Ability of Pilots to Control Simulated Short-Period Yawing Oscillations
Phillips, William H. & Cheatham, Donald C.
November 13, 1950
Primary view of The Absorption and Translocation of Several Fission Elements by Russian Thistle
Selders, A. A.
June 8, 1950
Primary view of Abstracts of the Literature Synthesis of Apatites and Some Related Phosphates: Part 1
Jaffe, Elizabeth B.
December 1950
Primary view of Advanced Seminar in Reactor Physics
Smith, Nicholas M.
July 26, 1950
Primary view of Aerodynamic and Lateral-Control Characteristics of a 1/28-Scale Model of the Bell X-1 Airplane Wing-Fuselage Combination: Transonic-Bump Method
Lockwood, Vernard E.
May 5, 1950
Primary view of Aerodynamic Characteristics at a Mach Number of 1.25 of a 6-Percent-Thick Triangular Wing and 6- and 9-Percent-Thick Triangular Wings in Combination With a Fuselage: Wing Aspect Ratio 2.31, Biconvex Airfoil Sections
Hall, Albert W. & Morris, Garland J.
May 5, 1950
Primary view of Aerodynamic Characteristics at a Mach Number of 1.38 of Four Wings of Aspect Ratio 4 Having Quarter-Chord Sweep Angles of 0 Degrees, 35 Degrees, 45 Degrees, and 60 Degrees
Kemp, William B., Jr.; Goodson, Kenneth W. & Booth, Robert A.
October 10, 1950
Primary view of Aerodynamic characteristics at Reynolds numbers of 3.0 x 10(exp 6) and 6.0 x 10(exp 6) of three airfoil sections formed by cutting off various amounts from the rear portion of the NACA 0012 airfoil section
Smith, Hamilton A. & Schaefer, Raymond F.
April 1950
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 a wing with unswept quarter-chord line, aspect ratio 2, taper ratio 0.78, and NACA 65A004 airfoil section: transonic-bump method
Polhamus, Edward C. & Campbell, George S.
March 8, 1950
Primary view of Aerodynamic characteristics of a wing with unswept quarter-chord line, aspect ratio 4, taper ratio 0.6, and NACA 65A004 airfoil section: Transonic-bump method
Myers, Boyd C., II & Wiggins, James W.
May 8, 1950
Primary view of Aerodynamic Characteristics of Damping Screens
Schubauer, G. B.; Spangenberg, W. G. & Klebanoff, P. S.
January 1950
Primary view of Aerodynamic characteristics of NACA RM-10 missile in 8- by 6-foot supersonic wind tunnel at Mach numbers from 1.49 to 1.98 1: presentation and analysis of pressure measurements (stabilizing fins removed)
Luidens, Roger W. & Simon, Paul C.
July 20, 1950
Primary view of Aerodynamic characteristics of NACA RM-10 missile in 8- by 6-foot supersonic wind tunnel at Mach numbers from 1.49 to 1.98 2: presentation and analysis of force measurements
Esenwein, Fred T.; Obery, Leonard J. & Schueller, Carl F.
July 21, 1950
Primary view of Aerodynamic characteristics of NACA RM 10 missile in 8 by 6 foot supersonic wind tunnel at Mach numbers from 1.49 to 1.98. 3: analysis of force distribution at angle of attack (stabilizing fins removed)
Luidens, Roger W. & Simon, Paul C.
December 12, 1950
Primary view of Aerodynamic characteristics with fixed and free transition of a modified delta wing in combination with fuselage at high subsonic speeds
Polhamus, Edward C. & King, Thomas J., Jr.
May 2, 1950
Primary view of Aerodynamic coefficients for an oscillating airfoil with hinged flap, with tables for a Mach number of 0.7
Turner, M. J. & Rabinowitz, S.
October 1950
Primary view of The aerodynamic forces and moments on a 1/10-scale model of a fighter airplane in spinning attitudes as measured on a rotary balance in the Langley 20-foot free-spinning tunnel
Stone, Ralph W., Jr.; Burk, Sanger M., Jr. & Bihrle, William, Jr.
September 1950
Primary view of The Aerodynamic Forces on Slender Plane- and Cruciform-Wing and Body Combinations
Spreiter, John R.
1950%
Primary view of Aerodynamic Investigation of a Parabolic Body of Revolution at Mach Number of 1.92 and Some Effects of an Annular Jet Exhausting From the Base
Love, Eugene S.
February 8, 1950
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