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Primary view of 11,400 KW Nuclear Power Plant Employing an Organic Moderated Reactor: Preliminary Description
Wheelock, C. W.
1957
Primary view of 15 MW Gas-Cooled Closed-Cycle Reactor Power System Study: Final Report, Volumes 1-2
unknown creator
April 1, 1957
Primary view of 20,000 KW Nuclear Power Plant Study for United States Atomic Energy Commission
Gilbert Associates, Inc.
July 7, 1957
Primary view of Abnormal grain growth in M-252 and S-816 alloys
Decker, R F; Rush, A I; Dano, A G & Freeman, J W
November 1957
Primary view of Abnormal grain growth in nickel-base heat-resistant alloys
Decker, R F; Rush, A I; Dano, A G & Freeman, A G
December 1957
Primary view of Accelerations in fighter-airplane crashes
Acker, Loren W; Black, Duglad O & Moser, Jacob C
November 4, 1957
Primary view of Accidents from explosives at metal and nonmetallic mines
Cash, Frank E.
1957
Primary view of Additional experiments with flat-top wing- body combinations at high supersonic speeds
Gloria, H. R.; Syvertson, C. A. & Wong, T. J.
February 19, 1957
Primary view of Aerodynamic and hydrodynamic characteristics of a proposed supersonic multijet water-based hydro-ski aircraft with a variable-incidence wing
Petynia, William W.; Hasson, Dennis F. & Spooner, Stanley H.
October 23, 1957
Primary view of Aerodynamic characteristics at high speeds of related full-scale propellers having different blade-section cambers
Maynard, Julian D & Salters, Leland B , Jr
1957?
Primary view of Aerodynamic characteristics at Mach number of 4.06 of a typical supersonic airplane model using body and vertical-tail wedges to improve directional stability
Dunning, Robert W
December 3, 1957
Primary view of Aerodynamic Characteristics of a 0.04956-Scale Model of the Convair TF-102A Airplane at Transonic Speeds, Coord. No. AF-120
Osborne, Robert S.
1957~
Primary view of The aerodynamic characteristics of a body in the two-dimensional flow field of a circular-arc wing at a Mach number of 2.01
Gapcynski, John P & Carlson, Harry W
July 2, 1957
Primary view of Aerodynamic characteristics of a circular cylinder at Mach number 6.86 and angles of attack up to 90 degrees
Penland, Jim A
January 1957
Primary view of Aerodynamic characteristics of a model of an escape capsule for a supersonic bomber-type airplane at a Mach number of 2.49
Presnell, John G , Jr
December 3, 1957
Primary view of Aerodynamic characteristics of missile configurations with wings of low aspect ratio for various combinations of forebodies, afterbodies, and nose shapes for combined angles of attack and sideslip at a Mach number of 2.01
Robinson, Ross B
June 25, 1957
Primary view of Aerodynamic Forces and Moments on a Large Ogive-Cylinder Store at Various Locations Below the Fuselage Center Line of a Swept-Wing Bomber Configuration at a Mach Number of 1.61
Morris, O. A.
January 14, 1957
Primary view of Aerodynamic Forces on a Vibrating Unstaggered Cascade
Soehngen, H.
August 1957
Primary view of Aerodynamic Heating and Boundary-layer Transition on a 1/10-power nose shape in free flight at Mach numbers up to 6.7 and Free-stream Reynolds numbers up tp 16 x 10(exp 6)
Garland, Benjamine J; Swanson, Andrew G & Speegle, Katherine C
June 17, 1957
Primary view of Aerodynamic heating of a thin, unswept, untapered, multiweb, aluminum-alloy wing at Mach numbers up to 2.67 as determined from a free-flight investigation of a rocket-propelled model
Strass, H Kurt & Stephens, Emily W
August 6, 1957
Primary view of Aerodynamic interference of slender wing-tail combinations
Sacks, Alvin H
January 1957
Primary view of Aerodynamic load distribution over a 45 degree swept wing having a spoiler-slot-deflector aileron and other spoiler ailerons for Mach numbers from 0.60 to 1.03
West, F E , Jr; Whitcomb, Charles F & Schmeer, James W
December 5, 1957
Primary view of Aerodynamic Loads on Tails at High Angles of Attack and Sideslip
Polhamus, E. C. & Spahr, J. R.
July 23, 1957
Primary view of Aerodynamic performance of several techniques for spike-position control of  a blunt-lip nose inlet having internal contraction; Mach numbers of 0.63 and 1.5 to 2.0
Anderson, Arthur A & Weinstein, Maynard I
September 17, 1957