PKK Library Search for 'au:" Czarnecki, K. R."'

PRESSURE DISTRIBUTION DUE TO TWO-DIMENSIONAL FABRICATION-TYPE SURFACE ROUGHNESS ON AN TRANSONIC SPEEDS

By Czarnecki,K. R.. Nasa, Washington, D.C. 1966 . 78 , Bound With Nasa Tn D-3516-20

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PRESSURE DRAGS DUE TO TWO-DIMENSIONAL FABRICATION-TYPE SURFACE ROUGHNESS ON AN OGIVE CYLINDER AT TRANSONIC SPEEDS

By Czarnecki,K. R.. Nasa, Washington, D.C. 1966 . 54 , Bound With Nasa Tn D-3519-20

Place Hold on PRESSURE DRAGS DUE TO TWO-DIMENSIONAL FABRICATION-TYPE SURFACE ROUGHNESS ON AN OGIVE CYLINDER AT TRANSONIC SPEEDS

THEORETICAL PRESSURE DISTRIBUTIONS OVER ARBITRARILY SHAPED PERIODIC WAVES IN SUBSONIC COMORESSIBLE FLOW AND COMPARISON WITH EXPERIMENT

By Czarnecki,K. R.. Nasa, Washington, D.C. 1970 . 33 , Bound With Nasa Tnd-5980-89

Place Hold on THEORETICAL PRESSURE DISTRIBUTIONS OVER ARBITRARILY SHAPED PERIODIC WAVES IN SUBSONIC COMORESSIBLE FLOW AND COMPARISON WITH EXPERIMENT

DRAG DUE TWO-DIMENSIONAL SURFACE ROUGHNESS IN A TURBULENT BOUNDRY LAYER AT MACH 3 WITH AND WITHOUT HEAT TRANSFER

By Monta,William J., Czarnecki,K. R.. Nasa, Washington, D.C. 1968 . 39 , Bound With Nasa Tnd 4741-4750

Place Hold on DRAG DUE TWO-DIMENSIONAL SURFACE ROUGHNESS IN A TURBULENT BOUNDRY LAYER AT MACH 3 WITH AND WITHOUT HEAT TRANSFER

EFFECTS AT MACH NUMBERS OF 1.61 AND 2.01 OF CAMBER AND TWIST ON THE AERODYNAMIC CHARACTERISTICS OF THREE SWEPT WINGS HAVING THE SAME PLANFORM

By Landrum,Emma Jean. Nasa, Washington, D.C. 1961 . 48 , Bound With Nasa Tn D-921-30

Place Hold on EFFECTS AT MACH NUMBERS OF 1.61 AND 2.01 OF CAMBER AND TWIST ON THE AERODYNAMIC CHARACTERISTICS OF THREE SWEPT WINGS HAVING THE SAME PLANFORM

EFFECT OF FABRICATION-TYPE SURFACE ROUGHNESS ON TRANSITION ON OGIVE-CYLINDER MODELS AT MACH NUMBERS OF 1.61 AND 2.01

By Howard,Paul W. Nasa, Washington, D.C. 1963 . 48 , Bound With Nasa Tn D-1931-40

Place Hold on EFFECT OF FABRICATION-TYPE SURFACE ROUGHNESS ON TRANSITION ON OGIVE-CYLINDER MODELS AT MACH NUMBERS OF 1.61 AND 2.01

Roughness drag due to two-dimensional fabrication type surface roughness on an ogive cylinder from force tests at transonic speeds [NASA TN D-5004]

By Czarnecki, K. R.. Washington, D.C. NASA 1959 . 45p

Place Hold on Roughness drag due to two-dimensional fabrication type surface roughness on an ogive cylinder from force tests at transonic speeds [NASA TN D-5004]

EFFECTS OF NOSE BLUNTNESS ON TRANSITION FOR A CONE AND A HOLLOW CYLINDER AT MACH NUMBERS 1.41 AND 2.01.

By Monta,William J,Howard,Paul W. Nasa, Washington, D.C. 1961 . 34 , Bound With Nasa Tn D-701-16, 718-20

Place Hold on EFFECTS OF NOSE BLUNTNESS ON TRANSITION FOR A CONE AND A HOLLOW CYLINDER AT MACH NUMBERS 1.41 AND 2.01.

EFFECTS OF CONE ANGLE, MACH NUMBER, AND NOSE BLUNTING ON TRANSITION AT SUPERSONIC SPEEDS [NASA TN D-634]

By Czarnecki, K. R.. Washington, D.C. National aeronautics and Space Administration 1961 . 31p , Bound vol. contains with NASA TN D 631-640

Place Hold on EFFECTS OF CONE ANGLE, MACH NUMBER, AND NOSE BLUNTING ON TRANSITION AT SUPERSONIC SPEEDS [NASA TN D-634]

BOUNDARY-LAYER VELOCITY PROFILES AND SKIN FRICTION DUE TO SURFACE ROUGHNESS ON AN OGIVE CYLINDER AT MACH NUMBERS OF 1.61 AND 2.01

By Czarnecki,K R. Nasa, Washington, D.C. 1963 . 40 , Bound With Nasa Tn D-2041-47, 2049-50

Place Hold on BOUNDARY-LAYER VELOCITY PROFILES AND SKIN FRICTION DUE TO SURFACE ROUGHNESS ON AN OGIVE CYLINDER AT MACH NUMBERS OF 1.61 AND 2.01

Pressure distributions and wave drag due to two-dimensional fabrication-type surface roughness on an ogive cylinder at mach numbers of 1.61 and 2.01 [NASA TN D-835]

By Czarnecki, K. R.. Washington, D.C. Nasa 1961 . 78p ,

Place Hold on Pressure distributions and wave drag due to two-dimensional fabrication-type surface roughness on an ogive cylinder at mach numbers of 1.61 and 2.01 [NASA TN D-835]

ANALYTICAL INVESTIGATION OF REDUCTION IN TURBULENT SKIN FRICTION ON A FLAT PLATE BY MEANS OF AIR INJECTION THROUGH DISCRETE SLOTS

By Czarnecki,K R. Nasa, Washington, D.C. 1964 . 59 , Bound With Nasa Tn D-2101,2103-2110

Place Hold on ANALYTICAL INVESTIGATION OF REDUCTION IN TURBULENT SKIN FRICTION ON A FLAT PLATE BY MEANS OF AIR INJECTION THROUGH DISCRETE SLOTS

DRAG REDUCTION DUE TO GAS INJECTION THROUGH VARIOUS DISCRETE SLOTS ON A THREE-DIMENSIONAL WING AT MACH 2.01

By Sorrells Iii,Russell B,Czarnecki,K R. Nasa, Washington, D.C. 1969 . 43 , Bound With Nasa Tn D-5300-5306,5308-5310

Place Hold on DRAG REDUCTION DUE TO GAS INJECTION THROUGH VARIOUS DISCRETE SLOTS ON A THREE-DIMENSIONAL WING AT MACH 2.01

EVALUATION OF BOUNDARY-LAYER AND WAKE-SURVEY DATA-REDUCTION TECHNIQUES IN COMPRESSIBLE FLOWS

By CZARNECKI,K R. NASA, WASHINGTON, D.C. 1968 . ,31,,,,,, , Bound with NASA TN D-4402-10

Place Hold on EVALUATION OF BOUNDARY-LAYER AND WAKE-SURVEY DATA-REDUCTION TECHNIQUES IN COMPRESSIBLE FLOWS

Investigation by schliern technique of methods of fixing fully turbulent floe on models at supersonic speed [NASA TN D-242]

By Jackson, Mary W. and Czarnecki, K. R.. Washington, D. C. NASA 1960 . 16p

Place Hold on Investigation by schliern technique of methods of fixing fully turbulent floe on models at supersonic speed [NASA TN D-242]

Measurment by wake momentum surveys at mach 1.61 and 2.01 of turbulent boundary-layer skin friction on five swept wings[NASA TN D3764]

By Sorrells,Russell.B.. Washington,D.C. National Aeronautics And Space Administration 1966 . 28p

Place Hold on Measurment by wake momentum surveys at mach 1.61 and 2.01 of turbulent boundary-layer skin friction on five swept wings[NASA TN D3764]

NASA Technical Note [D-2701-2710]

Washington National Aeronautics and Space Administration (NASA) 1965 , NASA TN D-2701: Effects of Lateral control, characteristics on hovering: jet lift vtol aircraft/ by L. Stewart Rolls, Fred J. Drinkwater III and Robert C. Innis | NASA TN D-2702: Impact of V / STOL aircraft on instrument weather operations/ John P. Reeder | NASA TN D-2703: Description and initial calibration of the langley 12-inch Hypersonic ceramic-heated tunnel/ Louis E. Clark | NASA TN D-2704: Hemispherical spectral emittance of ablation chars, carbon, and zirconia to 3700 degree K / by R. Gale Wilson | NASA TN D-2705: results of USAF-NASA-FAA flight program to study community responses to sonic booms in the greater St. Louis Area/ by Charles W. Nixon, Harvey H. Hubbard | NASA TN D-2706: Effect of surface emittance on turbulent skin friction at supersonic and low hypersonic speeds/ Jerry M. Allen and K. R. Czarnecki | NASA TN D-2707: Fixed- base simulator study of piloted entry into the earth's atmosphere at parabolic velocity/ by Martin T. Moul and Albert A. Schy | NASA TN D-2708: Study of pressure and heat transfer over an 80 degree sweep slab delta wing in hypersonic flow/ Allen H. Whitehead and James C. Dunavant | NASA TN D-2709: Effect of first-stage geometry on aerdynamic characteristics in pitch of two-stage rocket vehicles from mach 1.57 to 2.86/ by William A. Corlett and Celia S. Richardson | NASA TN D-2710: Effect of combined linear and oscillatory acceleration on pilot attitude-control capabilities/by Constantine B. Dolkas and John D. Stewart

Place Hold on NASA Technical Note [D-2701-2710]