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Primary view of Average Outside-Surface Heat-Transfer Coefficients and Velocity Distributions for Heated and Cooled Impulse Turbine Blades in Static Cascades
Hubbartt, James E. & Schum, Eugene F.
March 9, 1951
Primary view of Investigations toward simplification of missile control systems
Curfman, Howard J., Jr.; Strass, H. Kurt & Crane, Harold L.
November 12, 1953
Primary view of Comparison of the performance of a helicopter-type ram-jet engine under various centrifugal loadings
Radin, Edward J. & Carpenter, Paul J.
October 7, 1953
Primary view of Large-scale low-speed wind-tunnel tests of a model having a 60 degree delta horizontal canard control surface and wing to obtain static-longitudinal-stability and canard surface hinge-moment data
Burrows, Dale L.
June 17, 1954
Primary view of Wind-Tunnel Investigation to Determine the Horizontal- and Vertical-Tail Contributions to the Static Lateral Stability Characteristics of a Complete-Model Swept-Wing Configuration at High Subsonic Speeds
Wiggins, James W.; Kuhn, Richard E. & Fournier, Paul G.
July 10, 1953
Primary view of Rocket-Model Investigation to Determine the Hinge-Moment and Normal-Force Properties of a Full-Span, Constant-Chord, Partially Balanced Trailing-Edge Control on a 60 Degree Clipped Delta Wing Between Mach Numbers of 0.50 and 1.26
Martz, C. William & Goslee, John W.
October 30, 1953
Primary view of A pressure-distribution investigation of a fineness-ratio-12.2 parabolic body of revolution (NACA RM-10) at M = 1.59 and angles of attack up to 36 degrees
Cooper, Morton; Gapcynski, John P. & Hasel, Lowell E.
October 30, 1952
Primary view of A study of the use of various high-lift devices on the horizontal tail of a canard airplane model as a means of increasing the allowable center-of-gravity travel
Johnson, Joseph L., Jr.
January 21, 1953
Primary view of The Effects of a Small Jet of Air Exhausting From the Nose of a Body of Revolution in Supersonic Flow
Love, Eugene S.
November 12, 1952
Primary view of Investigation of the Aerodynamic Characteristics of the NACA RM-10 Missile (With Fins) at a Mach Number of 1.62 in the Langley 9-Inch Supersonic Tunnel
Coletti, Donald E.
December 19, 1952
Primary view of An experimental study of five annular air inlet configurations at subsonic and transonic speeds
Pendley, Robert E.; Milillo, Joseph R.; Fleming, Frank F. & Bryan, Carroll R.
August 19, 1953
Primary view of Wind-Tunnel Investigation at Low Speed of a Wing Having 63 Degree Sweepback and a Drooped Tip
Blackaby, James R.
April 7, 1955
Primary view of Development of a new flutter testing technique using a towed dynamic airplane model equipped with an automatic stabilizing system: Experimental and calculated dynamic stability characteristics for speeds up to 200 mph
Schneider, William C.
March 25, 1955
Primary view of Simulator studies of a simple homing system
Passera, Anthony L. & Garner, H. Douglas
October 6, 1955
Primary view of An Investigation of Loads on Ailerons at Transonic Speeds
Runckel, Jack F. & Gray, W. H.
May 27, 1955
Primary view of Wind-Tunnel Investigation at Low Speed of Sideslipping, Rolling, Yawing, and Pitching Characteristics for a Model of a 45 Degree Swept-Wing Fighter-Type Airplane
Jaquet, Byron M. & Fletcher, H. S.
September 1, 1955
Primary view of An Experimental Investigation of the Flow Phenomena Over Bodies at High Angles of Attack at a Mach Number of 2.01
Gapcynski, John P.
October 27, 1955
Primary view of Wing-load measurements at supersonic speeds of the Douglas D-558-II research airplane
Robinson, Glenn H.; Cothren, George E., Jr. & Pembo, Chris
March 30, 1955
Primary view of Statistical measurements of landing contact conditions of the Boeing B-47 airplane
Kolnick, Joseph J. & Morris, Garland J.
October 27, 1955
Primary view of Modified tubular combustor as high-temperature gas generators
Friedman, Robert & Zettle, Eugene V.
October 21, 1955
Primary view of An experimental investigation of the unsteady lift induced on a wing in the downwash field of an oscillating canard control surface
Reese, David E., Jr.
August 15, 1955
Primary view of Estimation of Incremental Pitching Moments Due to Trailing-Edge Flaps on Swept and Triangular Wings
James, Harry A. & Hunton, Lynn W.
June 10, 1955
Primary view of Aerodynamic heating of rocket-powered research vehicles at hypersonic speeds
Piland, Robert O. & Collie, Katherine A.
July 19, 1955
Primary view of Simplified procedures for estimating flap-control loads at supersonic speeds
Czarnecki, K. R. & Lord, Douglas R.
May 27, 1955
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