PKK Library Search for 'au:"Maglieri, Domenic J."'

PRELIMINARY MEASUREMENT OF THE THE NOISE CHARACTERISTICS OF SOME JET-AUGMENTED CONFIGURATIONS

By Maglieri,Domenic J, Hubbard,Harvey H. Nasa, Washington, D.C. 1959 . 46 , Bound With Nasa Memo 12-1-58l-12-31-58l

Place Hold on PRELIMINARY MEASUREMENT OF THE THE NOISE CHARACTERISTICS OF SOME JET-AUGMENTED CONFIGURATIONS

NASA Technical Note [NASA TN D-3443]: Ground measurements of shock-wave pressure for fighter airplanes flying at very low altitudes and comments on associated response phenomena

Washington NASA 1966 . 63p , Bound together NASA TN D-3441 to 3450 | Bound vol. Acc. No. 64324 contains Acc. No. TR8886 to TR8894

Place Hold on NASA Technical Note [NASA TN D-3443]: Ground measurements of shock-wave pressure for fighter airplanes flying at very low altitudes and comments on associated response phenomena

GROUND MEASUREMENTS OF THE SHOCK-WAVE NOISE FROM AIRPLANES IN LEVEL FLIGHT AT MACH NUMBERS TO 1.4 AND AT ALTITUDES TO 45,000 FEET [NASA TN D-48]

By Maglieri, Domenic J.. Washington, D.C. National Aeronautics and Space Admiistration 1959 . 38p , Bounds vol.contains NASA TN D-41-50

Place Hold on GROUND MEASUREMENTS OF THE SHOCK-WAVE NOISE FROM AIRPLANES IN LEVEL FLIGHT AT MACH NUMBERS TO 1.4 AND AT ALTITUDES TO 45,000 FEET [NASA TN D-48]

WIND-TUNNEL INVESTIGATION OF THE EFFECT OF ANGLE OF ATTACK AND FLAPPING-HINGE OFFSET ON PERIODIC BENDING MOMENTS AND FLAPPING OF A SMALL ROTOR

By Mccarty,John Locke,Brooks,George W. Nasa, Washington, D.C. 1959 . 44 , Bound With Nasa Memo 3-2-59l, Nasa Memo 3-4-59l-3-17-59l

Place Hold on WIND-TUNNEL INVESTIGATION OF THE EFFECT OF ANGLE OF ATTACK AND FLAPPING-HINGE OFFSET ON PERIODIC BENDING MOMENTS AND FLAPPING OF A SMALL ROTOR

THE SHOCK-WAVE NOISE PROBLEM OF SUPERSONIC AIRCRAFT IN STEADY FLIGHT

By Maglieri,Domenic J. Nasa, Washington, D.C. 1959 . 15 , Bound With Tr007387-88, Tr007390-98

Place Hold on THE SHOCK-WAVE NOISE PROBLEM OF SUPERSONIC AIRCRAFT IN STEADY FLIGHT

In-flight shock-wave pressure measurements above and below a bomber airplane at Mach numbers from 1.42 to 1.69 [NASA TN D-1968]

By Maglieri, Domenic J.. Washington, D.C. National Aeronautics and Space Administration [NASA] 1963 . 46p , Bound with NASA TN D-1961-1970. Lack No.-1966

Place Hold on In-flight shock-wave pressure measurements above and below a bomber airplane at Mach numbers from 1.42 to 1.69 [NASA TN D-1968]

Ground measurements of the shock wave noise from supersonic bomber airplanes in the altitude range from 30,000 to 50,000 feet [NASA TN D-880]

By Maglieri, Domenic J.. Washington, D. C. NASA 1961 . 24p

Place Hold on Ground measurements of the shock wave noise from supersonic bomber airplanes in the altitude range from 30,000 to 50,000 feet [NASA TN D-880]

Sonic-boom measurements during bomber training operations in the chicago area [NASA TN D-3655]

By Hilton, David A.. Washington, D.C. National Aeronautics and Space Administration 1966 . 26p

Place Hold on Sonic-boom measurements during bomber training operations in the chicago area [NASA TN D-3655]

NASA Technical Note [NASA TN D-1941]: Measurements of the response of two light airplanes

Washington NASA 1963 . 35p , Bound together NASA TN D-1941 to 1950 | Bound vol. Acc. No. 65584 contains Acc. No. TR10692 to TR10700

Place Hold on NASA Technical Note [NASA TN D-1941]: Measurements of the response of two light airplanes