Dryden Technical Report Server
From NTRS: Locate an electronic (PDF) copy of the document.
- LANDING LOADS AND ACCELERATIONS OF THE XB-70-1 AIRPLANE , Technical Note
Authors: R. J. Wilson and J. M. McKay
Report Number: NASA-TN-D-4836
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Abstract: Landing loads and accelerations of the XB-70-1 aircraft.
Distribution/Availability: Unclassified - Unlimited
Subject Category: 05
Availability:
Format(s) on-line:
PDF (1,411 KBytes)
Report Date: October 1968
No. Pages: 29
Keywords: Acceleration (physics); B-70 aircraft; Center of gravity; Landing gear; Landing loads.
- EVALUATION OF LATERAL-DIRECTIONAL HANDLING QUALITIES OF PILOTED REENTRY VEHICLES UTILIZING A FIXED BASE SIMULATION , Technical Note
Authors: F. J. Van Leynseele
Report Number: NASA-TN-D-4410
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Abstract: Flight simulator to evaluate lateral-directional handling qualities of piloted reentry vehicles.
Distribution/Availability: Unclassified - Unlimited
Subject Category: 15
Availability:
From NTRS: Locate an electronic (PDF) copy of the document.
Report Date: March 1968
No. Pages: 34
Keywords: Controllability; Flight simulators; Lateral stability; Lifting reentry vehicles; Roll.
- A REVIEW OF TRANSPORT HANDLING-QUALITIES CRITERIA IN TERMS OF PRELIMINARY XB-70 FLIGHT EXPERIENCE , Technical Memorandum
Authors: B. G. Powers
Report Number: NASA-TM-X-1584
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Abstract: Flight tests for preliminary evaluation of handling qualities of unaugmented XB-70 aircraft.
Distribution/Availability: Unclassified - Unlimited
Subject Category: 05
Availability:
Format(s) on-line:
PDF (1,150 KBytes)
Report Date: May 1968
No. Pages: 34
Keywords: B-70 aircraft; Flight characteristics; Flight tests; Lateral control; Longitudinal control.
- ADVANCED AIR DATA SENSING TECHNIQUES , Technical Memorandum
Authors: R. K. Bogue and L. D. Webb
Report Number: NASA-TM-X-61115
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Abstract: X-15 flight test data on fluidic temperature sensor for measuring total temperature of hypersonic aircraft.
Distribution/Availability: Unclassified - Unlimited
Subject Category: 35
Availability:
Format(s) on-line:
PDF (1,310 KBytes)
Report Date: January 1968
No. Pages: 33
Keywords: Flight tests; Fluid flow; Hypersonic aircraft; Temperature measuring instruments; X-15 aircraft.
Notes: PRESENTED AT THE 5TH INTERN. AEROSPACE INSTR. SYMP., CRANFIELD, ENGLAND, 25-28 MAR. 1968.
- ATMOSPHERIC CONDITIONS ASSOCIATED WITH TURBULENCE ENCOUNTERED BY THE XB-70 AIRPLANE ABOVE 40,000 FEET ALTITUDE , Technical Note
Authors: L. J. Ehernberger
Report Number: NASA-TN-D-4768
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Abstract: Atmospheric conditions during turbulences encountered by XB-70 aircraft above 40,000 ft.
Distribution/Availability: Unclassified - Unlimited
Subject Category: 46
Availability:
From NTRS: Locate an electronic (PDF) copy of the document.
Report Date: September 1968
No. Pages: 49
Keywords: Atmospheric temperature; Atmospheric turbulence; B-70 aircraft; Stratosphere; Wind variations.
- PRELIMINARY MEASURED AND PREDICTED XB-70 ENGINE NOISE , Technical Memorandum
Authors: P. L. Lasagna and N. J. McLeod
Report Number: NASA-TM-X-1565
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Abstract: B-70 aircraft engine noise measurements and predictions.
Distribution/Availability: Unclassified - Unlimited
Subject Category: 05
Availability:
Format(s) on-line:
PDF (1,142 KBytes)
Report Date: April 1968
No. Pages: 21
Keywords: Acoustic measurement; B-70 aircraft; Data reduction; Engine noise; J-93 engine.
- PRELIMINARY FLIGHT EVALUATION OF THE STABILITY AND CONTROL DERIVATIVES AND DYNAMIC CHARACTERISTICS OF THE UNAUGMENTED XB-70-1 AIRPLANE INCLUDING COMPARISONS WITH PREDICTIONS , Technical Note
Authors: C. H. Wolowicz, L. W. Strutz, G. B. Gilyard and N. W. Matheny
Report Number: NASA-TN-D-4578
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Abstract: Aerodynamic stability and control characteristics of supersonic aircraft.
Distribution/Availability: Unclassified - Unlimited
Subject Category: 05
Availability:
Format(s) on-line:
PDF (2,496 KBytes)
Report Date: May 1968
No. Pages: 78
Keywords: Aerodynamic stability; Aircraft performance; Flight characteristics; Flight tests; Supersonic aircraft.
- RECORDING AND SIGNAL-CONDITIONING TECHNIQUES AND EQUIPMENT USED IN A 1,000-FLIGHT BIOMEDICAL STUDY , Technical Note
Authors: R.Carpenter and J. Roman
Report Number: NASA-TN-D-4487
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Abstract: Signal conditioning methods and equipment used for inflight recording of pilot biomedical data.
Distribution/Availability: Unclassified - Unlimited
Subject Category: 52
Availability:
From NTRS: Locate an electronic (PDF) copy of the document.
Report Date: April 1968
No. Pages: 17
Keywords: Airborne equipment; Data recording; Flight stress (biology); Physiological effects; Pilot performance.
- FM HANDLING AND ANALOG-TO-DIGITAL CONVERSION OF BIOMEDICAL DATA FROM A 1,000-FLIGHT STUDY , Technical Note
Authors: R. Carpenter and J. Roman
Report Number: NASA-TN-D-4488
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Abstract: FM data handling facility for preparing analog physiological data obtained in flight for digital computations.
Distribution/Availability: Unclassified - Unlimited
Subject Category: 52
Availability:
From NTRS: Locate an electronic (PDF) copy of the document.
Report Date: April 1968
No. Pages: 12
Keywords: Airborne equipment; Analog to digital converters; Data systems; Flight stress (biology); Frequency modulation.
- BASE PRESSURE MEASUREMENTS ON THE XB-70 AIRPLANE AT MACH NUMBERS FROM 0.4 TO 3.0 , Technical Memorandum
Authors: Edwin J. Saltzman, Sheryll A. Goecke and Chris Pembo
Report Number: NASA-TM-X-1612
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Abstract: Base pressure measurements on XB-70 aircraft at Mach numbers from 0.4 to 3.0.
Distribution/Availability: Unclassified - Unlimited
Subject Category: 05
Availability:
Format(s) on-line:
PDF (2,024 KBytes)
Report Date: September 1968
No. Pages: 36
Keywords: Aerodynamic characteristics; Aerodynamic coefficients; B-70 aircraft; Base pressure; Pressure measurement.
- FLOW-FIELD INVESTIGATIONS ON THE X-15 AIRPLANE AND MODEL UP TO HYPERSONIC SPEEDS , Technical Note
Authors: L. J. McLain and M. Palitz
Report Number: NASA-TN-D-4813
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Abstract: Flow distribution in flight test and wind tunnel hypersonic flow of X-15 aircraft.
Distribution/Availability: Unclassified - Unlimited
Subject Category: 02
Availability:
Format(s) on-line:
PDF (1,382 KBytes)
Report Date: September 1968
No. Pages: 33
Keywords: Aircraft models; Flight tests; Flow distribution; Hypersonic flow; X-15 aircraft.
- A METHOD FOR THE SURFACE INSTALLATION AND FAIRING OF STATIC-PRESSURE ORIFICES ON A LARGE SUPERSONIC-CRUISE AIRPLANE , Technical Memorandum
Authors: N. V. Taillon
Report Number: NASA-TM-X-1530
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Abstract: Installation and fairing of flush, static pressure orifices on wing surfaces of supersonic aircraft.
Distribution/Availability: Unclassified - Unlimited
Subject Category: 02
Availability:
Format(s) on-line:
PDF (1,614 KBytes)
Report Date: March 1968
No. Pages: 12
Keywords: Aerodynamic characteristics; Fairings; Pressure gages; Static pressure; Supersonic aircraft.
- X-15 ANALOG AND DIGITAL INERTIAL SYSTEMS FLIGHT EXPERIENCE , Technical Note
Authors: M. E. Burke
Report Number: NASA-TN-D-4642
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Abstract: Analog and digital inertial flight data systems for X-15 aircraft.
Distribution/Availability: Unclassified - Unlimited
Subject Category: 59
Availability:
From NTRS: Locate an electronic (PDF) copy of the document.
Report Date: July 1968
No. Pages: 22
Keywords: Analog computers; Analog data; Digital navigation; Inertial navigation; X-15 aircraft.
- HEAT TRANSFER EFFECTS OF SURFACE PROTUBERANCES ON THE X-15 AIRPLANE , Technical Memorandum
Authors: Joe D. Watts and Frank V. Olinger
Report Number: NASA-TM-X-1566
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Abstract: No abstract available.
Distribution/Availability: Unclassified - Unlimited
Subject Category: 01
Availability:
Format(s) on-line:
PDF (1,053 KBytes)
Report Date: May 1968
No. Pages: 29
Keywords: Heat transfer; Separated flow; Skin temperature (biology); Turbulent flow; X-15 aircraft.
- NONLINEAR TIME-DOMAIN MODELS OF HUMAN CONTROLLERS , Technical Memorandum
Authors: L. W. Taylor, Jr.
Report Number: NASA-TM-X-60996
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Abstract: Applicability of nonlinear time domain analysis to problem of modeling human operator /pilot/
Distribution/Availability: Unclassified - Unlimited
Subject Category: 51
Availability:
Format(s) on-line:
PDF (611 KBytes)
Report Date: January 1968
No. Pages: 19
Keywords: Linear prediction; Mathematical models; Nonlinearity; Operator performance; Pilot performance.
Notes: PRESENTED AT HAWAII INTERN. CONF. ON SYSTEM SCI., HONOLULU, HAWAII, 29-31 JAN. 1968.
- A PRELIMINARY FLYING-QUALITIES EVALUATION OF A VARIABLE-SWEEP FIGHTER-TYPE AIRCRAFT , Technical Memorandum
Authors: T. R. Sisk, N. W. Matheny, D. A. Kier and J. A. Manke
Report Number: NASA-TM-X-1583
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Abstract: No abstract available.
Distribution/Availability: Unclassified - Unlimited
Subject Category: 01
Availability:
Format(s) on-line:
PDF (1,424 KBytes)
Report Date: May 1968
No. Pages: 42
Keywords: Aircraft control; Boundary value problems; Fighter aircraft; Flight characteristics; Variable sweep wings.
- METEOROLOGICAL ASPECTS OF HIGH-ALTITUDE TURBULENCE ENCOUNTERED BY THE XB-70 AIRPLANE , Technical Memorandum
Authors: L. J. Ehernberger
Report Number: NASA-TM-X-61114
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Abstract: Meteorological aspects of high altitude turbulence encountered by XB-70 aircraft.
Distribution/Availability: Unclassified - Unlimited
Subject Category: 05
Availability:
Format(s) on-line:
PDF (478 KBytes)
Report Date: May 1968
No. Pages: 9
Keywords: Atmospheric turbulence; B-70 aircraft; Flight; High altitude; Turbulence effects.
Notes: PRESENTED AT THE AIAA 3RD NATL. CONF. ON AEROSPACE METEOROLOGY, NEW ORLEANS, 6-9 MAY 1968.
- FLIGHT SIMULATION OF NIGHT LANDINGS OF LIFTING ENTRY VEHICLES. , Conference Paper
Authors: M. O. Thompson and W. H. Dana
Report Number: H-511
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Abstract: Lifting entry vehicles night landing flight simulation by night approaches and landings of piloted fighter aircraft with low L/D ratio.
Distribution/Availability: Unclassified - Unlimited
Subject Category: 05
Availability:
From NTRS: Locate an electronic (PDF) copy of the document.
Report Date: March 1968
No. Pages: 9
Keywords: Aircraft landing; Fighter aircraft; Horizontal spacecraft landing; Landing simulation; Lifting reentry vehicles.
Notes: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, FLIGHT TEST, SIMULATION AND SUPPORT CONFERENCE, 2ND, LOS ANGELES, CALIF., MAR. 25-27, 1968. AIAA PAPER 68-259.
- FLIGHT TESTING OF ADVANCED SPACECRAFT RECOVERY CONCEPTS USING THE AEROMODELER'S APPROACH , Conference Paper
Authors: R. D. Reed
Report Number: H-512
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Abstract: Advanced spacecraft recovery flight tests using radio controlled model airplane techniques involving gliding parachute models launched from carrier models.
Distribution/Availability: Unclassified - Unlimited
Subject Category: 15
Availability:
From NTRS: Locate an electronic (PDF) copy of the document.
Report Date: March 1968
No. Pages: 8
Keywords: Flight tests; Horizontal spacecraft landing; Lifting reentry vehicles; Spacecraft models; Spacecraft recovery.
Notes: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, FLIGHT TEST, SIMULATION AND SUPPORT CONFERENCE, 2ND, LOS ANGELES, CALIF., MAR. 25-27, 1968. AIAA PAPER 68-242.
- WIND-TUNNEL CALIBRATION OF A 40 DEG CONICAL PRESSURE PROBE AT MACH NUMBERS FROM 3.5 TO 7.4 , Technical Note
Authors: F. W. Burcham, Jr.
Report Number: NASA-TN-D-4678
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Abstract: Wind tunnel calibration of conical pressure probe over range of Mach numbers to determine flow field data for X-15 airplane.
Distribution/Availability: Unclassified - Unlimited
Subject Category: 34
Availability:
Format(s) on-line:
PDF (1,287 KBytes)
Report Date: July 1968
No. Pages: 26
Keywords: Flow distribution; Mach number; Pressure sensors; Wind tunnel calibration; X-15 aircraft.
- A SIMPLE LABORATORY METHOD FOR REDUCTION OF RHYTHM AND RATE IN LARGE-SCALE MONITORING OF ELECTROCARDIOGRAM , Technical Note
Authors: J. Roman, F. M. Larmie and T. R. Figarola
Report Number: NASA-TN-D-4751
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Abstract: Rapid reduction method of rhythm and rate information in large scale electrocardiogram monitoring.
Distribution/Availability: Unclassified - Unlimited
Subject Category: 52
Availability:
From NTRS: Locate an electronic (PDF) copy of the document.
Report Date: August 1968
No. Pages: 15
Keywords: Arrhythmia; Electrocardiography; Playbacks; Signal analysis; Waveforms.
Notes: PREPARED IN COOPERATION WITH NORTHROP CORP. AND LOVELACE FOUND. FIELD TEAMS AT EDWARDS, CALIF.
- INVESTIGATION OF THE CONTROLLABILITY OF THE M2-F2 LIFTING-BODY LAUNCH FROM THE B-52 CARRIER AIRPLANE , Technical Memorandum
Authors: B. M. Kock and W. D. Painter
Report Number: NASA-TM-X-1713
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Abstract: Air launch characteristics of M2-F2 lifting body from B-52 aircraft.
Distribution/Availability: Unclassified - Unlimited
Subject Category: 15
Availability:
From NTRS: Locate an electronic (PDF) copy of the document.
Report Date: December 1968
No. Pages: 33
Keywords: Aerodynamic characteristics; Air launching; Aircraft control; Aircraft performance; Aircraft safety.
- PRELIMINARY FLIGHT INVESTIGATION OF DYNAMIC PHENOMENA WITHIN AIR BREATHING PROPULSION SYSTEMS OF SUPERSONIC AIRCRAFT , Conference Paper
Authors: R. H. Smith, D. R. Bellman and D. L. Hughes
Report Number: H-518
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Abstract: F-111A and XB-70A aircraft instrumentation systems used to investigate dynamic response within air breathing propulsion systems of supersonic aircraft.
Distribution/Availability: Unclassified - Unlimited
Subject Category: 07
Availability:
From NTRS: Locate an electronic (PDF) copy of the document.
Report Date: June 1968
No. Pages: 10
Keywords: Aerodynamic characteristics; Air breathing engines; Aircraft engines; Aircraft instruments; B-70 aircraft.
Notes: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, PROPULSION JOINT SPECIALIST CONFERENCE, 4TH, CLEVELAND, OHIO, JUN. 10-14, 1968. AIAA PAPER 68-593.
- USE OF STRAIN GAGES FOR MEASUREMENTS OF FLIGHT LOADS IN A HIGH-TEMPERATURE ENVIRONMENT , Conference Paper
Authors: E. J. Wilson
Report Number: H-521
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Abstract: Strain gages to measure flight loads in high temperature environment, discussing selection, calibration techniques and performance characteristics.
Distribution/Availability: Unclassified - Unlimited
Subject Category: 35
Availability:
From NTRS: Locate an electronic (PDF) copy of the document.
Report Date: January 1968
No. Pages: 5
Keywords: Calibrating; Conferences; Flight load recorders; High temperature environments; Strain gages.
Notes: INSTRUMENT SOCIETY OF AMERICA, ANNUAL TEST MEASUREMENT SYMPOSIUM, 5TH, NEW YORK, N.Y., OCT. 28-31, 1968, PROCEEDINGS. P. 555 1- 555 5. /ADVANCES IN TEST MEASUREMENT. VOLUME 5
- FLIGHT AND LABORATORY TESTING OF A DOUBLE SIDEBAND FM TELEMETRY SYSTEM , Technical Memorandum
Authors: R. B. Richardson and P. F. Harney
Report Number: NASA-TM-X-56015
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Abstract: Double sideband suppressed carrier FM telemetry system as airborne data recorder, discussing noise, environmental conditions, laboratory and flight tests.
Distribution/Availability: Unclassified - Unlimited
Subject Category: 32
Availability:
Format(s) on-line:
PDF (600 KBytes)
Report Date: July 1968
No. Pages: 18
Keywords: Airborne equipment; Double sideband transmission; Frequency modulation; Signal to noise ratios; Telemetry.
Notes: INTERNATIONAL TELEMETERING CONFERENCE, LOS ANGELES, CALIF., OCT. 8-11, 1968, PROCEEDINGS. P. 581-596. CONFERENCE SPONSORED BY THE INTERNATIONAL FOUNDATION FOR TELEMETERING.
- FLIGHT EXPERIENCE WITH SHOCK IMPINGEMENT AND INTERFERENCE HEATING ON THE X-15-2 RESEARCH AIRPLANE , Technical Memorandum
Authors: Joe D. Watts
Report Number: NASA-TM-X-1669
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Abstract: Severe structural melting damage due to complex shock impingement and interference effects on local aerodynamic heating was experienced on a flight of the X-15-2 research airplane to a maximum Mach number of 6.7. Measured flight temperature data and observed structural damage resulting from shock impingement and interference heating on the airplane and its ablative coating were analyzed in the light of hypersonic wind-tunnel results. The best approximations of the flight results were made by increasing the undisturbed pylon leading-edge heat-transfer coefficient by a factor of 9 and the undisturbed heat-transfer coefficient in the two interference zones by a factor of 7. The calculated effect of increased heat transfer due to interference n radiation-equilibrium temperature is presented for selected hypersonic cruise conditions.
Distribution/Availability: Unclassified - Unlimited
Subject Category: 05
Availability:
Format(s) on-line:
PDF (2,286 KBytes)
Report Date: October 1968
No. Pages: 27
Keywords: Aerodynamic heating; Aerodynamic interference; Aircraft structures; Damage assessment; Heat transfer.
- MEASUREMENT OF THE XB-70A PROPULSION PERFORMANCE INCORPORATING THE GAS GENERATOR METHOD , Conference Paper
Authors: W. Beaulieu, R. Campbell and W. Burcham
Report Number: H-526
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Abstract: Propulsion performance of XB-70A aircraft calculated by gas generator method.
Distribution/Availability: Unclassified - Unlimited
Subject Category: 07
Availability:
From NTRS: Locate an electronic (PDF) copy of the document.
Report Date: June 1968
No. Pages: 9
Keywords: B-70 aircraft; Conferences; Gas generators; Propulsion system performance; Turbojet engines.
Notes: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, PROPULSION JOINT SPECIALIST CONFERENCE, 4TH, CLEVELAND, OHIO, JUN. 10-14, 1968. AIAA PAPER 68-594.
- VERTICAL-TAIL LOADS AND CONTROL-SURFACE HINGE-MOMENT MEASUREMENTS ON THE M2-F2 LIFTING BODY DURING INITIAL SUBSONIC FLIGHT TESTS , Technical Memorandum
Authors: J. M. Jenkins, M. H. Tang and G. P. E. Pearson
Report Number: NASA-TM-X-1712
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Abstract: Vertical tail loads and control surface hinge moment measurements on M2-F2 lifting body at subsonic speeds.
Distribution/Availability: Unclassified - Unlimited
Subject Category: 39
Availability:
Format(s) on-line:
PDF (1,737 KBytes)
Report Date: December 1968
No. Pages: 25
Keywords: Aerodynamic characteristics; Aerodynamic loads; Control surfaces; Flight tests; M-2F2 lifting body.
- PREDICTED AND MEASURED XB-70 GROUND-TO-GROUND ENGINE NOISE
Authors: N. J. McLeod, P. L. Lasagna and T. W. Putnam
Report Number: H-532
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Abstract: Predicted and measured ground noise effects of B-70 aircraft engine.
Distribution/Availability: Unclassified - Unlimited
Subject Category: 71
Availability:
From NTRS: Locate an electronic (PDF) copy of the document.
Report Date: January 1968
No. Pages: 12
Keywords: B-70 aircraft; Ground effect (aerodynamics); Jet aircraft noise; Noise intensity; Performance prediction.
Notes: IN ITS PROGR. OF NASA RES. RELATING TO NOISE ALLEVIATION OF LARGE SUBSONIC JET AIRCRAFT 1968 P 423-434. NASA SP-189.
- LESSONS FROM THE XB-70 AS APPLIED TO THE SUPERSONIC TRANSPORT , Technical Memorandum
Authors: F. L. Fulton, Jr.
Report Number: NASA-TM-X-56014
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Abstract: XB-70 aircraft flight test data as applied to supersonic transports.
Distribution/Availability: Unclassified - Unlimited
Subject Category: 05
Availability:
Format(s) on-line:
PDF (1,469 KBytes)
Report Date: January 1968
No. Pages: 19
Keywords: Aircraft design; B-70 aircraft; Controllability; Flight tests; Hydraulic equipment.
Notes: PRESENTED AT THE 21ST ANN. INTERN. AIR SAFETY SEMINAR, ANAHEIM, CALIF., 7-11 OCT. 1968.
|
