Showing 1 - 20 results of 26 for search 'Purser, Paul E.', query time: 0.07s
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1
Wind-tunnel tests at low speed of swept and yawed wings having various plan forms / by Purser, Paul E.
Published 1951Call Number: Loading…
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2
Wind-tunnel investigation of a plain aileron with thickened and beveled trailing edges on a tapered low-drag wing / by Purser, Paul E.
Published 1943Call Number: Loading…
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3
Comparison of pitching moments produced by plain flaps and by spoilers and some aerodynamic characteristics of an NACA 23012 airfoil with various types of aileron / by Purser, Paul E.
Published 1945Call Number: Loading…
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4
Experimental verification of a simplified vee-tail theory and analysis of available data on complete modes with vee-tails / by Purser, Paul E.
Published 1945Call Number: Loading…
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5
Wind-tunnel investigation of the characteristics of blunt-nose ailerons on a tapered wing / by Purser, Paul E.
Published 1943Call Number: Loading…
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6
Aerodynamic characteristics and flap loads of the brake-flap installation on the 0.40-scale model of the F4F-3 left wing panel / by Purser, Paul E.
Published 1942Call Number: Loading…
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7
Wind-tunnel investigation of an NACA 23012 airfoil with a 0.30-airfoil-chord double slotted flap / by Purser, Paul E.
Published 1942Call Number: Loading…
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8
Wind-tunnel investigation of perforated split flaps for use as dive brakes on a tapered NACA 23012 airfoil / by Purser, Paul E.
Published 1941Call Number: Loading…
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9
Analysis of available data on control surfaces having plain-overhang and Frise balances / by Purser, Paul E.
Published 1944Call Number: Loading…
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10
Effects of trailing-edge modifications on pitching moment characteristics of airfoils / by Purser, Paul E.
Published 1944Call Number: Loading…
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11
A study of the application of data on various types of flap to the design of fighter brakes / by Purser, Paul E.
Published 1942Call Number: Loading…
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12
Aerodynamic characteristics and flap loads of perforated double split flaps on a rectangular NACA 23012 airfoil / by Purser, Paul E.
Published 1943Call Number: Loading…
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13
Wind-tunnel investigation of perforated split flaps for use as dive brakes on a rectangular NACA 23012 airfoil / by Purser, Paul E.
Published 1941Call Number: Loading…
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14
Collection and analysis of hinge-moment data on control-surface tabs / by Purser, Paul E.
Published 1947Call Number: Loading…Search for the full-text version of this title in HathiTrust
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15
Preliminary investigation at low speed of downwash characteristics of small-scale sweptback wings / by Purser, Paul E.
Published 1947Call Number: Loading…
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16
Tests to determine effects of slipstream rotation on the lateral stability characteristics of a single-engine low-wing airplane model / by Purser, Paul E.
Published 1946Call Number: Loading…
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17
Wind-tunnel investigation of effects of unsymmetrical horizontal-tail arrangements on power-on static longitudinal stability of a single-engine airplane model / by Purser, Paul E.
Published 1947Call Number: Loading…
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18
Manned spacecraft : engineering design and operation / by Purser, Paul E.
Published 1965Call Number: Loading…
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19
Wind-tunnel investigation of 20-percent-chord plain and Frise ailerons on an NACA 23012 airfoil / by Rogallo, Francis M. (Francis Melvin), 1912-2009
Published 1941Other Authors: “…Purser, Paul E.…”
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20
Wind-tunnel investigation of control-surface characteristics. : 14 - NACA 0009 airfoil with a 20-percent-chord double plain flap / by Sears, Richard I.
Published 1943Other Authors: “…Purser, Paul E.…”
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Related Subjects
Charts, diagrams, etc
Airplanes
Wind tunnel testing
Aerofoils
Flaps (Airplanes)
Ailerons
Control surfaces
Control
Split flaps (Airplanes)
Wings
Tabs (Airplanes)
Trailing edges (Aerodynamics)
Aerodynamic load
Air flow
Hinge moments (Aerodynamics)
Aerodynamics
Manned space flight
Models
Pitching (Aerodynamics)
Slotted flaps (Airplanes)
Stability of airplanes
Tail surfaces
Testing
Wakes (Aerodynamics)
Astronautics
Diving
Fighter planes
Measurement
Pressure
Reynolds number