PKK Library Search for 'au:"DAVENPORT,EDWIN E"'

EFFECTS OF GEOMETRIC VARIATIONS ON LIFT AUGMENTATION OF SIMPLE-PLENUM -CHAMBER GROUND-EFFECT MODELS

By Davenport,Edwin E. Nasa, Washington, D.C. 1961 . 20 , Bound With Nasa Tn D-751-60

Place Hold on EFFECTS OF GEOMETRIC VARIATIONS ON LIFT AUGMENTATION OF SIMPLE-PLENUM -CHAMBER GROUND-EFFECT MODELS

NASA Memo [10-13-58L]

By Petynia, William W.. Washington National Aeronautics and Space Administration 1960 . 59p , NASA Memorandum 10-1-58L-10-17-58L Bound Vol. No.102461; Contents: TR-8572-8580l

Place Hold on NASA Memo [10-13-58L]

TRANSITION CHARACTERISTICS OF A VTOL AIRCRAFT POWERED BY FOUR DUCTED TANDEM PROPELLERS

By Davenport,Edwin E. Nasa, Washington, D.C. 1964 . 55 , Bound With Nasa Tn D-2251-2253,2255-2260

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THRUST CHARACTERISTICS OF MULTIPLE LIFTING JETS IN GROUND PROXIMITY

By Davenport,Edwin E. Nasa, Washington, D.C. 1960 . 18 , Bound With Nasa Tn D-511-12,514-20

Place Hold on THRUST CHARACTERISTICS OF MULTIPLE LIFTING JETS IN GROUND PROXIMITY

STATIC LONGITUDINAL AERODYNAMIC CHRACTERISTICS OF SOME SUPERSONIC DECELERATOR MODELS AT MACH NUMBERS OF 2.30 AND 4.63.

By Davenport,Edwin E. Nasa, Washington, D.C. 1969 . 34 , Bound With Nasa Tn D-5211-5218.5220-5230.

Place Hold on STATIC LONGITUDINAL AERODYNAMIC CHRACTERISTICS OF SOME SUPERSONIC DECELERATOR MODELS AT MACH NUMBERS OF 2.30 AND 4.63.

INVESTIGATION OF THE AERODYNAMIC CHARACTERISTICS OF A COMBINATION JET-FLAP AND DEFLECTED-SLIPSTREAM CONFIGURATION AT ZERO AND LOW FORW ARD SPEEDS

By Spreemann,Kenneth P. Nasa, Washington, D.C. 1960 . 72 , Bound With Nasa Tn D-361-362,364-370

Place Hold on INVESTIGATION OF THE AERODYNAMIC CHARACTERISTICS OF A COMBINATION JET-FLAP AND DEFLECTED-SLIPSTREAM CONFIGURATION AT ZERO AND LOW FORW ARD SPEEDS

AERODYNAMIC CHARACTERISTICS OF THREE SLENDER SHARP-EDGE 74DEGREE SWEPT WINGS AT SUBSONIC,TRNSONIC,AND SUPERSONIC MACH NUMBERS.

By DAVENPORT,EDWIN E. NASA, WASHINGTON, D.C. 1974 . ,77,,,,,, , Bound with NASA TN D-7632-40.

Place Hold on AERODYNAMIC CHARACTERISTICS OF THREE SLENDER SHARP-EDGE 74DEGREE SWEPT WINGS AT SUBSONIC,TRNSONIC,AND SUPERSONIC MACH NUMBERS.

Effects of geometric variations on lift augmentation of simple-plenum-chamber ground effect models [NASA TR D751-TR D760]

By Davenport, Edwin E.. Washington National Aeronautics and Space Administration [NASA] 1961 . 20p

Place Hold on Effects of geometric variations on lift augmentation of simple-plenum-chamber ground effect models [NASA TR D751-TR D760]

Analysis of validation tests of the langley pilot transonic cryogenic tunnel [NASA TN D-7828]

Washington, D. C. National Aeronautics and Space Administration 1975 . 20p

Place Hold on Analysis of validation tests of the langley pilot transonic cryogenic tunnel [NASA TN D-7828]