182 Matching Results

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Primary view of Control characteristics at transonic speeds of a linked flap and spoiler on a tapered 45 degrees sweptback wing of aspect ratio 3
Lockwood, Vernard E. & Fikes, Joseph E.
July 11, 1952
Primary view of Flight measurements of the vibratory bending and torsion stress of a supersonic-type propeller for flight Mach numbers up to 0.95
O'Bryan, Thomas C.
July 11, 1956
Primary view of Flight measurements of the transonic drag of models of several isolated external stores and nacelles
Stevens, Joseph E. & Purser, Paul E.
March 11, 1955
Primary view of Flight tests of a two-dimensional wedge diffuser at transonic and supersonic speeds
Faget, M. A.
August 11, 1948
Primary view of Flight Measurements of the Stability Characteristics of the Bell X-5 Research Airplane in Sideslips at 59 Deg Sweepback
Childs, Joan M
February 11, 1953
Primary view of Investigation of a transonic turbine designed for a maximum rotor-blade suction-surface relative Mach number of 1.57
Whitney, Warren J.; Wong, Robert Y. & Monroe, Daniel E.
October 11, 1954
Primary view of Initial inclination of the mixing boundary separating an exhausting supersonic jet from a supersonic ambient stream
Love, Eugene S.
January 11, 1956
Primary view of Investigation of transient combustion characteristics in a single tubular combustor
Donlon, Richard H.; McCafferty, Richard J. & Straight, David M.
February 11, 1954
Primary view of Tests in the Ames 40- by 80-foot wind tunnel of an airplane configuration with an aspect ratio 2 triangular wing and an all-movable horizontal tail : lateral characteristics
Graham, David & Koenig, David G.
February 11, 1952
Primary view of Aerodynamic heating of a wing as determined from a free-flight rocket-model test to Mach number 3.64
Swanson, Andrew G. & Rumsey, Charles B.
September 11, 1956
Primary view of Preliminary empirical design requirements for the prevention of tumbling of airplanes having no horizontal tails
Bryant, Robert L.
October 11, 1950
Primary view of Preliminary analysis of a nuclear-powered supersonic airplane using ramjet engines
Weber, Richard J. & Connolley, Donald J.
April 11, 1958
Primary view of Preliminary investigation of an asymmetric swept nose inlet of circular projection at Mach number 3.85
Connors, James F. & Woollett, Richard R.
October 11, 1954
Primary view of Preliminary Results of Stability and Control Investigation of the Bell X-5 Research Airplane
Finch, Thomas W. & Briggs, Donald W.
February 11, 1953
Primary view of Longitudinal frequency-response characteristics of the Douglas D-558-I airplane as determined from experimental transient-response histories to Mach number of 0.90
Angle, Ellwyn E. & Holleman, Euclid C.
February 11, 1952
Primary view of Longitudinal stability and drag characteristics at Mach numbers from 0.75 to 1.5 of an airplane configuration having a 60 degree swept wing of aspect ratio 2.24 as obtained from rocket-propelled models
Vitale, A. James; McFall, John C., Jr. & Morrow, John D.
April 11, 1952
Primary view of Measured and estimated lateral static and rotary derivatives of a 1/12-scale model of a high-speed fighter airplane with unswept wings
Williams, James L.
January 11, 1954
Primary view of Free-spinning-tunnel investigation of a 1/28-scale model of the North American FJ-4 airplane: TED No. NACA AD-3112
Healy, Frederick M.
February 11, 1958
Primary view of Effect of flight speed on dynamics of a turboprop engine
Nakanishi, S.; Craig, R. T. & Wile, D. B.
April 11, 1955
Primary view of Effect of pressure level on afterburner-wall temperatures
Shillito, Thomas B. & Smolak, George R.
June 11, 1958
Primary view of Comparison of measured and predicted indicated angles of attack near the fuselages of a triangular-wing wind-tunnel model and a swept-wing fighter airplane in flight
McFadden, Norman M.; McCloud, John L., III & James, Harry A.
March 11, 1953
Primary view of Analysis of fully developed turbulent heat transfer at low Peclet numbers in smooth tubes with application to liquid metals
Deissler, Robert G
August 11, 1952
Primary view of Effect of inlet-annulus area blockage on over-all performance and stall characteristics of an experimental 15-stage axial-flow compressor
Lucas, James G.; Finger, Harold B. & Filippi, Richard E.
May 11, 1954
Primary view of Performance evaluation of reduced-chord rotor blading as applied to J23 two-stage turbine 6: stage performance with standard rotor blading at inlet conditions of 35 inches of mercury absolute and 700 degrees R
Davidson, Elmer H. & Schum, Harold J.
July 11, 1957