Technical Report Archive and Image Library (TRAIL) - 1,019 Matching Results

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Primary view of The Cladding of Delta-Phase Zirconium Hydride
Paprocki, Stan J.; Hodge, Edwin S. & Boyer, Charles B.
December 27, 1957
Primary view of Comparison and evaluation of two model techniques used in predicting bomb-release motions
Carlson, Harry W.; Geier, Douglas J. & Lee, John B.
December 27, 1957
Primary view of Comparison and Evaluation of Two Model Techniques Used in Predicting Bomb-Release Motions
Carlson, Harry W.; Geier, Douglas J. & Lee, John B.
December 27, 1957
Primary view of Experimental hinge moments on two freely oscillating trailing-edge controls hinged at 55 percent control chord
Martz, C. William
December 27, 1957
Primary view of Pressure measurements on an afterbody behind various blunt nose shapes at a Mach number of 2
Speegle, K. C.
December 27, 1957
Primary view of Supplementary investigation in the Langley 20-foot free-spinning tunnel of a 1/20-scale model of the Douglas F4D-1 airplane with external wing fuel tanks : TED No. NACA AD 3116
Bowman, James S , Jr
December 27, 1957
Primary view of Boron Isotope Enrichment: Pilot Plant Proposal for the Anisole - BF₃ System
Hambrock, Kenneth O. & Miller, George T.
December 23, 1957
Primary view of Design and economic study of hot off-gas storage system
Johnson, C. S. & Carter, T. J.
December 20, 1957
Primary view of Report of the Forty-Second National Conference on Weights and Measures, 1957
United States. National Bureau of Standards.
December 20, 1957
Primary view of Heat-Transfer and Pressure Measurements from a Flight Test of a 1/18-Scale Model of the Titan Intercontinental Ballistic Missile Up to a Mach Number of 3.95 and Reynolds Number Per Foot of 23 by 10 to the 6th Power
Graham, John B., Jr.; Chauvin, Leo T. & Speegle, Katherine C.
December 19, 1957
Primary view of Heat-transfer and pressure measurements from a flight test of a 1/18-scale model of the Titan intercontinental ballistic missile up to a Mach number of 3.95 and Reynolds number per foot of 23 x 10(exp 6): COORD. No. AF-AM-70
Graham, John B., Jr.; Chauvin, Leo T. & Speegle, Katherine C.
December 19, 1957
Primary view of Delta-Phase Zirconium Hydride as a Solid Moderator
Vetrano, James B.
December 18, 1957
Primary view of The effects of boundary-layer separation over bodies of revolution with conical tail flares
Dennis, David H.
December 12, 1957
Primary view of Experimental investigation of the simulation of atmospheric entry of ballistic missiles
Neice, Stanford E.; Carson, James A. & Cunningham, Bernard E.
December 12, 1957
Primary view of In-flight gains realized by modifying a twin side-inlet induction system
Saltzman, Edwin J
December 12, 1957
Primary view of In-flight Gains Realized by Modifying a Twin Side-inlet Induction System
Saltzman, E. J.
December 12, 1957
Primary view of An investigation of the control effectiveness of tip ailerons and spoilers on a low-aspect-ratio trapezoidal-wing airplane model at Mach numbers from 1.55 to 2.35
Wong, Norman D
December 12, 1957
Primary view of Theoretical and experimental investigation of arbitrary aspect ratio, supercavitating hydrofoils operating near the free water surface
Johnson, Virgil E., Jr.
December 12, 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 Flight investigation of the transonic longitudinal and lateral handling qualities of the Douglas X-3 research airplane
Fischel, Jack; Holleman, Euclid C & Tremant, Robert A
December 5, 1957
Primary view of Investigation at high subsonic speeds of the use of low auxiliary tail surfaces having dihedral to improve the longitudinal and directional stability of a T-tail model at high lift
Sleeman, William C., Jr.
December 5, 1957
Primary view of Normal-force and hinge-moment characteristics at transonic speeds of flap-type ailerons at three spanwise locations on a 4-percent-thick sweptback-wing-body model and pressure distribution measurements on an inboard aileron
Runckel, Jack F. & Hieser, Gerald
December 5, 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 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