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1.
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PRESSURE DISTRIBUTION DUE TO TWO-DIMENSIONAL FABRICATION-TYPE SURFACE ROUGHNESS ON AN TRANSONIC SPEEDS
by Czarnecki,K. R | Monta,William J. Material type: Book Description: 78.Publisher: Nasa, Washington, D.C. 1966Availability: No items available
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2.
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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 | Monta,William J. Material type: Book Description: 54.Publisher: Nasa, Washington, D.C. 1966Availability: No items available
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3.
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THEORETICAL PRESSURE DISTRIBUTIONS OVER ARBITRARILY SHAPED PERIODIC WAVES IN SUBSONIC COMORESSIBLE FLOW AND COMPARISON WITH EXPERIMENT
by Czarnecki,K. R | Jackson,Mary W. Material type: Book Description: 33.Publisher: Nasa, Washington, D.C. 1970Availability: No items available
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4.
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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 | Deveikis,William D. Material type: Book Description: 39.Publisher: Nasa, Washington, D.C. 1968Availability: No items available
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5.
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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 | Czarnecki,K R. Material type: Book Description: 48.Publisher: Nasa, Washington, D.C. 1961Availability: No items available
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6.
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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 | Czarnecki,K R. Material type: Book Description: 48.Publisher: Nasa, Washington, D.C. 1963Availability: No items available
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7.
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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 | Monta, William J. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 45p.Publisher: Washington, D.C. NASA 1959Availability: No items available
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8.
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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 | Czarnecki,K R. Material type: Book Description: 34.Publisher: Nasa, Washington, D.C. 1961Availability: No items available
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9.
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EFFECTS OF CONE ANGLE, MACH NUMBER, AND NOSE BLUNTING ON TRANSITION AT SUPERSONIC SPEEDS [NASA TN D-634]
: National aeronautics and Space Administration
by Czarnecki, K. R | Jackson, Mary W. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 31p.Publisher: Washington, D.C. National aeronautics and Space Administration 1961Availability: No items available
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10.
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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 | Monta,William J. Material type: Book Description: 40.Publisher: Nasa, Washington, D.C. 1963Availability: No items available
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11.
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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 | Monta, William J. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 78p.Publisher: Washington, D.C. Nasa 1961Availability: No items available
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12.
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ANALYTICAL INVESTIGATION OF REDUCTION IN TURBULENT SKIN FRICTION ON A FLAT PLATE BY MEANS OF AIR INJECTION THROUGH DISCRETE SLOTS
by Czarnecki,K R. Material type: Book Description: 59.Publisher: Nasa, Washington, D.C. 1964Availability: No items available
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13.
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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 | Satchell,Lorraine F. Material type: Book Description: 43.Publisher: Nasa, Washington, D.C. 1969Availability: No items available
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14.
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EVALUATION OF BOUNDARY-LAYER AND WAKE-SURVEY DATA-REDUCTION TECHNIQUES IN COMPRESSIBLE FLOWS
:
by CZARNECKI,K R | SORRELLS,RUSSELL B. Material type: Book; Format:
print
; Nature of contents: Description: ,31.Publisher: NASA, WASHINGTON, D.C. 1968Availability: No items available
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15.
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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 | Czarnecki, K. R. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 16p.Publisher: Washington, D. C. NASA April 1960Availability: No items available
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16.
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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 | Jackson,Mary.W | Czarnecki,K.R. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 28p.Publisher: Washington,D.C. National Aeronautics And Space Administration 1966Availability: No items available
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17.
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NASA Technical Note [D-2701-2710]
by Rolls, L. Stewart Drinkwater III, Fred J. Innis, Robert C. Reeder, John P. Clark, Louis E. Wilson, R. Gale Nixon, Charles W. Hubbard, Harvey H. Allen, Jerry M. Czarnecki, K. R. Moul, Martin T. Schy, Albert A. Whitehead, Allen H. Dunavant, James C. Corlett, William A. and Richardson, Celia S. Dolkas, Constantine B. Stewart, John D. Material type: Book Publisher: Washington National Aeronautics and Space Administration (NASA) 1965Availability: No items available
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