Get started
Author

A I Neihouse

Observed names: A L Neihouse, Neihouse, A I, Neihouse, A. I., Neihouse, Anshal I.
OpenAlex ID: A5000744730
Tail-design requirements for satisfactory spin recovery for personal-owner-type light airplanes
1947 · A L Neihouse · 9
A Mass-Distribution Criterion for Predicting the Effect of Control Manipulation on the Recovery from a Spin
1942 · A I Neihouse · NASA Technical Reports Server (NASA) · 9
PDF
Dynamic Similitude Between a Model and a Full-Scale Body for Model Investigation at Full-Scale Mach Number
1950 · A I Neihouse, Philip W Pepoon · NASA STI Repository (National Aeronautics and Space Administration) · 7
PDF
Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails V : effect of airplane relative density
1940 · Oscar Seidman, A I Neihouse · NASA Technical Reports Server (NASA) · 4
Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails IV: effect of center-of-gravity location
1939 · Oscar Seidman, A I Neihouse · 2
Effect of current design trends on airplane spins and recoveries
1952 · A I Neihouse · 1
Free-spinning Wind-tunnel Tests of a Low-wing Monoplane with Systematic Changes in Wings and Tails III : Mass Distributed Along the Wings
1938 · Oscar Seidman, A I Neihouse · NASA Technical Reports Server (NASA) · 1
PDF
Langley research efforts on recovery systems
1962 · A I Neihouse · NASA Technical Reports Server (NASA)
PDF
Investigation to Determine the Effectiveness of a Split-Aileron Type Emergency Spin-Recovery Device for the Northrop XF-89 Airplane
1951 · A I Neihouse, H. A. Lee
NACA Research Memorandums
1951 · Neihouse, Anshal I., Klinar, Walter J., et al. · University of North Texas Digital Library (University of North Texas)
PDF
Spin-tunnel investigation to determine the effectiveness of a rocket for spin recovery
1949 · A I Neihouse · NASA Technical Reports Server (NASA)
The effect of variations in moments of inertia on spin and recovery characteristics of a single- engine low-wing monoplane with various tail arrangements, including a twin tail
1948 · A I Neihouse · NASA STI Repository (National Aeronautics and Space Administration)
NACA Advanced Restricted Reports
1942 · Neihouse, Anshal I., Pitkin, Marvin · University of North Texas Digital Library (University of North Texas)
PDF
The aileron as an aid to recovery from the spin
1940 · A I Neihouse · NASA Technical Reports Server (NASA)
PDF
NACA Technical Notes
1940 · Neihouse, Anshal I., Lichtenstein, Jacob H., et al. · University of North Texas Digital Library (University of North Texas)
PDF
NACA Technical Reports
1939 · Seidman, Oscar, Neihouse, A. I. · University of North Texas Digital Library (University of North Texas)
PDF
Comparison of free-spinning wind-tunnel results with corresponding full-scale spin results
1938 · A I Neihouse · NASA Technical Reports Server (NASA)
PDF
NACA Memorandum Reports
1938 · Seidman, Oscar, Neihouse, A. I. · University of North Texas Digital Library (University of North Texas)
PDF
Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails 3: mass distributed along the wings
1938 · Oscar Seidman, A I Neihouse
Free Spinning Wind-tunnel Tests of a Low-wing Monoplane with Systematic Wings and Tails
1937 · Oscar Seidman, A I Neihouse · NASA Technical Reports Server (NASA)
PDF
Free spinning wind-tunnel tests of a low-wing monoplane with systematic wings and tails 2: Mass distributed along the fuselage
1937 · Oscar Seidman, A I Neihouse
Free-spinning Wind-tunnel Tests of a Low-wing Monoplane with Systemic Changes in Wings and Tails
1937 · Oscar Seidman, A I Neihouse · NASA Technical Reports Server (NASA)
Free-spinning wind-tunnel tests of a low-wing monoplane with systemic changes in wings and tails 1: Basic loading condition
1937 · Oscar Seidman, A I Neihouse
Works count: 29
Citation count: 33
H-index: 4
I10-index:
Year
Topic
Type