National Advisory Committee for Aeronautics (NACA) - 183 Matching Results

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Primary view of Comparison of Calculated and Experimental Temperatures and Coolant Pressure Losses for a Cascade of Small Air-Cooled Turbine Rotor Blades
Stepka, Francis S.
September 4, 1958
Primary view of Comparison of Injectors With a 200-Pound-Thrust Ammonia-Oxygen Engine
Priem, Richard J. & Clark, Bruce J.
September 4, 1958
Primary view of Design and Experimental Performance of a 0.35 Hub-Tip Radius Ratio Transonic Axial-Flow-Compressor Rotor Designed for 40 Pounds Per Second Per Unit Frontal Area
Montgomery, John C. & Yasaki, Paul T.
September 4, 1958
Primary view of Thermal reaction of diborane with trimethylborane
Lamneck, John H., Jr. & Kaye, Samuel
September 4, 1958
Primary view of Aerodynamic Characteristics at a Mach Number of 6.8 of Two Hypersonic Missile Configurations, One With Low-Aspect-Ratio Cruciform Fins and Trailing-Edge Flaps and One With a Flared Afterbody and All-Movable Controls
Robinson, Ross B. & Bernot, Peter T.
August 4, 1958
Primary view of Aerodynamic Characteristics at a Mach Number of 6.8 of Two Hypersonic Missile Configurations, One With Low-Aspect-Ratio Cruciform Fins and Trailing-Edge Flaps and One With a Flared Afterbody and All-Movable Controls
Robinson, Ross B. & Bernot, Peter T.
August 4, 1958
Primary view of Aerodynamic characteristics at Mach numbers 2.36 and 2.87 of an airplane configuration having a cambered arrow wing with a 75 degree swept leading edge
Hallissy, Joseph M., Jr. & Hasson, Dennis F.
August 4, 1958
Primary view of Experimental and Analytical Investigation of the Transonic and Supersonic Divergence Characteristics of a Delta-Plan-Form All-Movable Control
Rainey, A. Gerald; Hanson, Perry W. & Martin, Dennis J.
August 4, 1958
Primary view of Flight investigation of the low-speed characteristics of a 45 degree swept-wing fighter-type airplane with blowing boundary-layer control applied to the trailing edge flaps
Quigley, Hervey C.; Anderson, Seth B. & Innis, Robert C.
August 4, 1958
Primary view of Effect of a hot-jet exhaust on pressure distributions and external drag of several afterbodies on a single-engine airplane model at transonic speeds
Norton, Harry T., Jr. & Swihart, John M.
March 4, 1958
Primary view of The effects of a modified roll-command system on the flight-path stability and tracking accuracy of an automatic interceptor
Triplett, William C.
March 4, 1958
Primary view of Static stability and control of canard configurations at Mach numbers from 0.70 to 2.22: lateral-directional characteristics of a triangular wing and canard
Peterson, Victor L. & Menees, Gene P.
March 4, 1958
Primary view of Study of exit phase of flight of a very high altitude hypersonic airplane by means of a pilot-controlled analog computer
Sherman, Windsor L.; Faber, Stanley & Whitten, James B.
March 4, 1958
Primary view of Accelerations in fighter-airplane crashes
Acker, Loren W.; Black, Dugald O. & Moser, Jacob C.
November 4, 1957
Primary view of A hydrogen peroxide turbojet-engine simulator for wing-tunnel powered-model investigations
Runckel, Jack F. & Swihart, John M.
November 4, 1957
Primary view of Transonic Flutter Investigation of Arrowhead Wing With Tip Ailerons and Trailing-Edge Flaps
Jones, George W., Jr. & Boswinkle, Robert W., Jr.
November 4, 1957
Primary view of The use of a leading-edge area-suction flap and leading-edge modifications to improve the high-lift characteristics of an airplane model with a wing of 45 degree sweep and aspect ratio 2.8
Koenig, David G. & Aoyagi, Kiyoshi
November 4, 1957
Primary view of Use of Constant Diffuser Mach Number as a Control Parameter for Variable-Geometry Inlets at Mach Numbers of 1.8 to 2.0
Hearth, Donald P. & Anderson, Bernhard H.
November 4, 1957
Primary view of Compressible Laminar Boundary Layer Over a Yawed Infinite Cylinder With Heat Transfer and Arbitrary Prandtl Number
Reshotko, Eli & Beckwith, Ivan E.
April 4, 1957
Primary view of Observation of Laminar Flow on an Air-Launched 15 Degree Cone-Cylinder at Local Reynolds Numbers to 50 X 10(Exp 6) at Peak Mach Number of 6.75
Rabb, Leonard & Krasnican, Milan J.
March 4, 1957
Primary view of Problem of Slip Flow in Aerodynamics
Street, Robert E.
March 4, 1957
Primary view of Reductions in Temperature-Recovery Factor Associated With Pulsating Flows Generated by Spike-Nosed Cylinders at a Mach Number of 3.50
Hermach, C. A.; Kraus, Samuel & Reller, John O., Jr.
March 4, 1957
Primary view of Some Data on Body and Jet Reaction Controls
Henning, Allen B.; Wineman, Andrew R. & Rainey, Robert W.
March 4, 1957
Primary view of Application of a Windshield-Display System to the Low-Altitude Bombing Problem
Barnett, Robert M.; Kauffman, William M. & Fulcher, Elmer C.
January 4, 1957
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